JPH0571613B2 - - Google Patents

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Publication number
JPH0571613B2
JPH0571613B2 JP25602889A JP25602889A JPH0571613B2 JP H0571613 B2 JPH0571613 B2 JP H0571613B2 JP 25602889 A JP25602889 A JP 25602889A JP 25602889 A JP25602889 A JP 25602889A JP H0571613 B2 JPH0571613 B2 JP H0571613B2
Authority
JP
Japan
Prior art keywords
film
vapor deposition
propylene
temperature
vapor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP25602889A
Other languages
Japanese (ja)
Other versions
JPH03115329A (en
Inventor
Katsuhiro Tsucha
Katsuya Ogawa
Masanao Hasegawa
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.)
Toray Industries Inc
Original Assignee
Toray Industries Inc
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 Toray Industries Inc filed Critical Toray Industries Inc
Priority to JP25602889A priority Critical patent/JPH03115329A/en
Publication of JPH03115329A publication Critical patent/JPH03115329A/en
Publication of JPH0571613B2 publication Critical patent/JPH0571613B2/ja
Granted legal-status Critical Current

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  • Laminated Bodies (AREA)
  • Shaping By String And By Release Of Stress In Plastics And The Like (AREA)
  • Physical Vapour Deposition (AREA)
  • Manufacture Of Macromolecular Shaped Articles (AREA)
  • Treatments Of Macromolecular Shaped Articles (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

〔産業上の利用分野〕 本発明は、蒸着用ポリプロピレンフイルムに関
する。さらに詳しくは、水蒸気や酸素などの気体
遮断性に優れた蒸着用ポリプロピレンフイルムに
関する。 〔従来の技術〕 従来、ポリプロピレンフイルムに表面処理を施
してアルミニウムなどの金属を蒸着したフイルム
が包装用途などに使用されている(例えば、特公
昭56−18381号公報など)。 〔発明が解決しようとする課題〕 従来の方法によつて得られた蒸着フイルムは、
蒸着接着強度が十分でなく、蒸着膜が摩耗で容易
に傷つき剥れたり、また、蒸着接着強度が十分で
ないと高温高湿下で蒸着膜が消失しやすく結果と
して蒸着フイルムの気体遮断性が悪化する。 また金属蒸着時にフイルムが熱を受けるため、
フイルムが微少寸法変化を起こし、蒸着膜が微少
クラツクを誘発するためか、蒸着フイルムの気体
遮断性が悪かつた。 本発明は、かかる問題点を改善し、蒸着接着強
度が強く、蒸着フイルムの気体遮断性に優れた、
蒸着用ポリプロピレンフイルムを提供することを
目的とする。 〔課題を解決するための手段〕 本発明は、ポリプロピレンフイルムの片面(A
面と略記する)の表層の原子構成比(酸素原子の
数/炭素原子の数)が0.10〜0.34、(窒素原子の
数/炭素原子の数)が0.005〜0.08の範囲にあり、
かつ、該フイルムの長さ方向の熱収開始温度が
105℃以上であることを特徴とする蒸着用ポリプ
ロピレンフイルムである。 本発明におけるポリプロピレンフイルムのポリ
マーはプロピレンの単独重合体が好ましいが、プ
ロピレンは他のα−オレフイン(例えばエチレ
ン、ブテン、ペンテンなど)との共重合体であつ
てもよい。共重合体を用いる場合、プロピレン成
分は95重量%以上が好ましい。プロピレン重合体
のアイソタクチツクインデツクス(I.I)は90以
上、好ましくは95以上が好ましい。極限粘度
[η]は1.2〜2.5dl/gの範囲にあるものが好ま
しい。 本発明ポリプロピレンフイルムの長さ方向にお
けるF5値(5%伸長時の応力)は4.0Kg/mm2以上、
好ましくは4.5Kg/mm2以上であると、気体遮断性
を向上することができるので好ましい。これは蒸
着あるいは、蒸着フイルムの後加工で張力による
フイルムの寸法変化を防止できることによる蒸着
膜のクラツク制御効果によるものである。 また本発明のポリプロピレンフイルムには、通
常用いられている、すべり剤、熱および酸化防止
剤、無機微粒子、帯電防止剤、増粘剤、減粘剤な
どの添加剤を添加してもよい。 本発明におけるA面表層の(酸素原子の数/炭
素原子の数)の比(以下「O/C」と略記する)
は、0.10〜0.34の範囲にあることが必要であり、
さらに好ましくは0.20〜0.30の範囲にあることが
望ましい。この範囲より小さい値になると、蒸着
接着強度が劣つたものとなつてしまう。また逆
に、この範囲より大きい値になると、フイルム表
層が脆くなる傾向が出てくるため、やはり接着強
度が低下してしまう。次に、(窒素原子の数/炭
素原子の数)の比(以下「N/C」と略記する)
は、0.005〜0.08の範囲にあることが必要であり、
さらに好ましくは、0.01〜0.05の範囲にあること
が望ましい。N/Cの値がこの範囲よりも小さい
値になると、蒸着接着強度が劣つたものとなり、
蒸着膜が摩耗で容易に傷つき、気体遮断性に劣つ
たものとなつてしまう。また逆に、この範囲より
大きい値になると接着性に劣つたものとなると同
時にフイルムがブロツキングする様になる。 本発明は、ポリプロピレンフイルムの表層(通
常、表面から10nm程度の深さまで極薄層)が、
酸素原子と窒素原子を上記した範囲内で同時に保
有していることが必要である。なお表層が酸素原
子のみを保有している場合、あるいは窒素原子の
みを保有している場合は、いずれも金属蒸着膜と
の接着性、耐摩耗性が劣つたものとなるので、気
体遮断性に優れた蒸着用フイルムに用いることは
極めて難しい。 また本発明におけるポリプロピレンフイルムの
長さ方向の熱収開始温度は105℃以上、好ましく
は110℃以上であることが必要である。熱収開始
温度が105℃未満、好ましくは110℃未満であると
気体遮断性が著しく悪化してしまう。この原因は
明確ではないが金属蒸着時の熱量によつて、フイ
ルムが微少寸法変化を起こし、蒸着界面で歪みが
発生し、蒸着膜にクラツクが発生するためと推測
される。 本発明においてA面の反対側面(以下「B面」
と略記する)にプロピレン・エチレン共重合体ま
たは/およびエチレン・プロピレン・ブテン共重
合体を積層して使用するのが好ましい。 これは金属蒸着時に、蒸着機の冷却ドラム(ク
ーリングキヤン)にプロピレン・エチレン共重合
体層あるいはエチレン・プロピレン・ブテン共重
合体層が密着して、冷却ドラム上で滑ることを防
止できるので、結果としてフイルムの熱寸法変化
量を減少でき、気体の遮断性を大幅に向上させる
ことができるのである。ここでプロピレン・エチ
レン共重合体としては、プロピレンにエチレンを
1〜7重量%ランダムに共重合させたものが好ま
しく、またエチレン・プロピレン・ブテン共重合
体としては、プロピレンにエチレン1〜5重量
%、ブテン3〜20重量%共重合したものが好まし
い。積層厚みは特に限定されないが1〜8μm、
気体遮断性と寸法安定性の点から1〜3.5μmが好
ましい。 次に、本発明のポリプロピレンフイルムの製造
法の一例を説明する。 押出機温度210〜280℃で、アイソタクチツクイ
ンデツクスが90%以上、極限年度[η]1.2〜2.5
dl/gのポリプロピレン樹脂を溶融し、スリツト
を施したTダイより、シート状に押出し、30〜90
℃の冷却ロールで冷却固化し未延伸シートとす
る。なおこの時必要に応じてもう一台の押出機よ
り、プロピレン・エチレン共重合体または/およ
びエチレン・プロピレン・ブテン共重合体を溶融
押出し、Tダイで積層し、積層未延伸シートとす
る。この未延伸シートを133〜144℃に加熱された
オーブンで加熱しながら、長さ方向に3〜6倍に
延伸し、次に幅方向に155〜165℃の温度で7〜12
倍に延伸し、幅方向に8.5〜12%のリラツクスを
施しながら155〜165℃の温度で熱処理をする。そ
の後、該フイルムを窒素と炭酸ガスの混合気体
(炭酸ガスの体積比0.5〜50%)の中に導き、フイ
ルム温度を40〜100℃、好ましくは45〜90℃に保
ちつつ、20〜120W・分/m2でA面をコロナ放電
処理を施し、製膜速度比100%未満の速度で巻取
る。 さらに、こうして得られたフイルムは、所定の
幅、長さにスリツトされるが、該スリツト時の長
さ方向張力も低い方が好ましい。 本発明の特性値の測定方法並びに効果の評価方
法は次の通りである。 (1) フイルム表層の原子構成比の測定法 島津製作所製のESCA750型を用い、フイル
ムの表面処理を、励起X線:MgK〓1,2線にして
光電子脱出角度90度、C1sメインピークの結合
エネルギー値を284.6eVに合わせて1s軸道の
ESCA測定し、得られたスペクトルから、C1s
のピークとO1sのピークの面積比を、(酸素原子
の数/炭素原子の数)の比、つまりO/Cの値
とし、またC1sのピークとN1sのピークの面積比
を、(窒素原子の数/炭素原子の数)の比、つ
まりN/Cの値とした。 (2) フイルム長さ方向熱収開始温度(℃) パーキン・エルマー社製熱機械的分析装置
(TMAシステム)を用い、フイルムから長さ
方向14mm、幅方向5mmの大きさの試料を採取
し、試長が10mmになるように、皺や傾きのない
様にセツトした後、フイルムの1mm2(断面積)
当り、40gの荷重をかけ、この試料を昇温開始
温度25℃から、10℃/分の昇温速度で昇温し、
縦軸に寸法変化率を、横軸に温度をとつて、加
熱寸法変化曲線を描いたとき、加熱寸法変化曲
線の寸法変化率0%軸との交点の温度(寸法変
化率が温度上昇とともに最初増大し、極大値を
経た後減少し再び0%となるときの温度)を熱
収開始温度とした。 第1図は、加熱寸法変化曲線の一例であり、
1は加熱寸法変化曲線、2は熱収開始温度であ
る。 (3) 気体遮断性 (A) 水蒸気透過率 JIS Z 208に準じて測定した。なおこの
とき蒸着面が塩化カルシウム側になる様にセ
ツトした。 (B) 酸素透過率 フイルムを常温常湿で1週間放置後、
ASTM−D−1434に準じ、モダンコントロ
ールズ社製OX−TRAN100型酸素透過率測
定装置を用いて酸素透過率を測定した。 (4) 蒸着接着強度 金属蒸着面に市販のセロフアン粘着テープ
(登録商標“セロテープ”)を貼合せ90°に剥離
したあとの金属付着残存面積で評価した。 残存面積 付着指数 95%以上 5 90%以上95%未満 4 75%以上90%未満 3 50%以上75%未満 2 50%未満 1 の基準で判定した。付着指数が高いほど接着力
が良好である。 (5) 蒸着面の耐摩耗性 蒸着面同志を荷重5g/cm2圧で10回摩擦し、
摩擦前後の光沢度差より下記の通りで判定し
た。 光沢度低下率(ΔG) =摩擦前の光沢度−10回摩擦時の光沢度/摩擦前の光
沢度 ○:ΔG≧0.95 △:0.85≦ΔG<0.95 ×:ΔG<0.85 (6) F5値 テンシロンを用いて、フイルム幅10mm、試長
100mmのサンプルを引張速度300mm/分の速度で
引張り、フイルムの5%伸長時の強力(Kg)を
フイルム断面積(mm2)で除した値で示した。 〔作用〕 本発明は、A面の表面を特定の原子構成比
(O/C、N/C)としたことにより、金属蒸着
膜が摩耗で傷ついたり剥れたりすることなく、蒸
着接着が強固となる。ここで注目すべきは、表面
に特定の原子構成比を持つと金属蒸着に際しポリ
プロピレン表層からにじみ出て、金属微結晶間の
分子間力を増加せしめることになるので、蒸着層
の金属微結晶相互の充填状態が密になり、その結
果、結晶欠陥やボイドの極めて少ない気体透過を
抑えることに有効である。 また、フイルム長さ方向の熱収開始温度を105
℃以上としたことにより、蒸着時での発熱による
フイルムの収縮寸法変化を抑え、金属蒸着クラツ
ク防止したことにより気体遮断性が改善できたも
のである。 〔実施例〕 本発明を実施例に基づいて説明する。 実施例 1 [η]が2.2dl/g、アイソタクチツクインデ
ツクスが96.5%のプロピレンホモポリマを、押出
機温度270℃で溶融押出し、40℃の冷却ドラムに
て冷却固化せしめて、未延伸シートを作つた。こ
のシートを141℃に加熱されたオーブンに通して
加熱しつつ、長手方向に5倍延伸した。次にこの
一軸延伸フイルムを115℃に加熱しながら3%の
リラツクスをした。続いて、163℃に加熱しつつ、
幅方向に9倍延伸し、幅方向に9.5%のリラツク
スを施しながら160℃で熱処理を行ない厚さ20μ
mの二軸延伸ポリプロピレンフイルムを作つた。
次いでこのフイルムの片面(A面)を、窒素と炭
酸ガスの混合気体(炭酸ガスの体積分率10%)中
で80℃に加熱しつつ、26W・分/m2でコロナ放電
処理し、巻取つた。該フイルムのO/C、N/
C、熱収開始温度を算出し、第1表に示した。さ
らに、このフイルムを、1000mm幅蒸着機にて300
m/分の速度でA面にアルミニウムを35nmの厚
みに蒸着した。蒸着フイルムの特性を第1表に示
す。 実施例 2 [η]が1.85dl/g、アイソタクチツクインデ
ツクスが97.5%のプロピレンホモポリマを、押出
温度260℃で溶融押出し、実施例1と同様にして
一軸延伸フイルムを作つた。次にこの一軸延伸フ
イルムを130℃で加熱しながら4.8%のリラツクス
を行なつた。続いて164℃に加熱しつつ、幅方向
に9倍延伸し、あとは実施例1とまつたく同様に
して二軸延伸ポリプロピレンフイルムを作つた。
次いで窒素と炭酸ガスの混合気体中で80℃に加熱
しつつ29W・分/m2でコロナ放電処理した。続い
て実施例1とまつたく同様にしてアルミニウム蒸
着を施した。フイルム特性を第1表に示した。 比較例 1〜3 実施例1と同様にして二軸延伸フイルムを作
り、コロナ放電処理強度を変更して第1表に示す
様なO/C、N/Cとした以外は、実施例1とま
つたく同様にアルミニウムを蒸着した。特性を第
1表に示す。 比較例 4 実施例1と同様にして二軸延伸フイルムを作成
し、次いでこのフイルムの片面(A面)を空気中
で65℃に加熱しつつ、24W・分/m2でコロナ放電
処理をし、実施例1と同様に巻取り、さらにこの
フイルムのA面に実施例1と同様に35nm厚みに
アルミニウム蒸着を実施した。特性を第1表に示
す。 比較例 5 [η]が2.2dl/g、アイソタクチツクインデ
ツクスが96.5%のプロピレンホモポリマを、押出
温度270℃で溶融押出し、40℃の冷却ドラムにて
冷却固化し、未延伸シートを作つた。このシート
を135℃に加熱されたオーブンに通して加熱しつ
つ、長手方向に5倍延伸した。次にこの一軸延伸
フイルムを110で2%のリラツクスを施し、続い
て162℃に加熱しつつ、幅方向に9倍延伸し、幅
方向に9.5%のリラツクスを施しながら155℃で熱
処理を行ない、厚さ20μmの二軸延伸ポリプロピ
レンフイルムを作つた。該フイルムを実施例1と
まつたく同様にして表面処理およびアルミニウム
蒸着を実施した。フイルム特性を第1表に示し
た。 実施例 3 一台の押出機から[η]1.85dl/g、アイソタ
チツクインデツクスが97.5%のプロピレンホモポ
リマを、押出温度260℃で溶融押出し、一方もう
一台の押出機より、エチレン・プロピレンランダ
ム共重合体(エチレン含有量3.7重量%)を溶融
押出し、口金で積層した。この時の二軸延伸フイ
ルムの厚みは、ポリプロピレン層16.5μm、プロ
ピレン・エチレン共重合体層3.5μmであつた。次
いで実施例1と同様にして二軸延伸、表面コロナ
処理、アルミニウム蒸着を行なつた。得られたフ
イルムの特性を第1表に示す。 第1表から明らかなように、実施例1、2、3
の本発明フイルムは、金属蒸着接着力が強く耐摩
耗性があり、気体遮断性(水蒸気透過率、酸素透
過率)に優れていることがわかる。 一方、比較例1〜4は表層の原子構成比が特定
範囲にないと、蒸着接着力、蒸着膜の耐摩耗性に
劣り、さらに気体遮断性に劣る。 また比較例5は熱収開始温度が低くなると、気
体遮断性の悪いものとなつた。
[Industrial Application Field] The present invention relates to a polypropylene film for deposition. More specifically, the present invention relates to a polypropylene film for deposition that has excellent barrier properties against gases such as water vapor and oxygen. [Prior Art] Conventionally, polypropylene films are surface-treated and metals such as aluminum are deposited on them for packaging purposes (for example, Japanese Patent Publication No. 18381/1981). [Problem to be solved by the invention] The vapor deposited film obtained by the conventional method is
If the vapor deposition adhesive strength is not sufficient, the vapor deposited film will be easily damaged and peeled off due to abrasion, and if the vapor deposition adhesive strength is not sufficient, the vapor deposited film will easily disappear under high temperature and high humidity, resulting in a deterioration of the gas barrier properties of the vapor deposited film. do. Also, since the film receives heat during metal deposition,
The gas barrier properties of the vapor-deposited film were poor, probably because the film underwent minute dimensional changes and the vapor-deposited film induced micro-cracks. The present invention improves these problems and provides a vapor-deposited film with strong adhesive strength and excellent gas barrier properties.
The purpose is to provide a polypropylene film for vapor deposition. [Means for Solving the Problems] The present invention provides one side of a polypropylene film (A
The atomic composition ratio (number of oxygen atoms/number of carbon atoms) of the surface layer (abbreviated as surface) is in the range of 0.10 to 0.34, (number of nitrogen atoms/number of carbon atoms) is in the range of 0.005 to 0.08,
and the temperature at which heat loss starts in the longitudinal direction of the film is
This is a polypropylene film for vapor deposition characterized by a temperature of 105°C or higher. The polymer of the polypropylene film in the present invention is preferably a propylene homopolymer, but propylene may also be a copolymer with other α-olefins (eg, ethylene, butene, pentene, etc.). When using a copolymer, the propylene component is preferably 95% by weight or more. The isotactic index (II) of the propylene polymer is preferably 90 or more, preferably 95 or more. The intrinsic viscosity [η] is preferably in the range of 1.2 to 2.5 dl/g. The F5 value (stress at 5% elongation) of the polypropylene film of the present invention in the longitudinal direction is 4.0 Kg/mm 2 or more,
Preferably, it is 4.5 Kg/mm 2 or more because gas barrier properties can be improved. This is due to the effect of controlling cracks in the vapor-deposited film by preventing dimensional changes in the film due to tension during vapor deposition or post-processing of the vapor-deposited film. The polypropylene film of the present invention may also contain commonly used additives such as slip agents, heat and antioxidant agents, inorganic fine particles, antistatic agents, thickeners, and thinners. The ratio (number of oxygen atoms/number of carbon atoms) of the A-side surface layer in the present invention (hereinafter abbreviated as "O/C")
must be in the range 0.10 to 0.34,
More preferably, it is in the range of 0.20 to 0.30. If the value is smaller than this range, the vapor deposition adhesive strength will be poor. Conversely, if the value is larger than this range, the surface layer of the film tends to become brittle, resulting in a decrease in adhesive strength. Next, the ratio (number of nitrogen atoms/number of carbon atoms) (hereinafter abbreviated as "N/C")
must be in the range 0.005 to 0.08,
More preferably, it is in the range of 0.01 to 0.05. When the N/C value is smaller than this range, the vapor deposition adhesive strength becomes inferior.
The deposited film is easily damaged by abrasion, resulting in poor gas barrier properties. On the other hand, if the value is larger than this range, the adhesiveness will be poor and at the same time the film will start to block. In the present invention, the surface layer of the polypropylene film (usually an extremely thin layer from the surface to a depth of about 10 nm)
It is necessary to simultaneously contain oxygen atoms and nitrogen atoms within the above range. Note that if the surface layer only contains oxygen atoms or only nitrogen atoms, the adhesion with the metal vapor deposited film and abrasion resistance will be poor, so the gas barrier properties will be poor. It is extremely difficult to use it as a good vapor deposition film. Further, in the present invention, the temperature at which heat loss begins in the longitudinal direction of the polypropylene film must be 105°C or higher, preferably 110°C or higher. If the heat loss start temperature is less than 105°C, preferably less than 110°C, gas barrier properties will be significantly deteriorated. Although the cause of this is not clear, it is presumed that the amount of heat during metal vapor deposition causes minute dimensional changes in the film, causing distortion at the vapor deposition interface and causing cracks in the vapor deposited film. In the present invention, the side opposite to side A (hereinafter referred to as “side B”)
It is preferable to use a propylene/ethylene copolymer or/and an ethylene/propylene/butene copolymer laminated on the (abbreviated as). This is because the propylene/ethylene copolymer layer or ethylene/propylene/butene copolymer layer adheres closely to the cooling drum (cooling can) of the vapor deposition machine during metal deposition, preventing it from slipping on the cooling drum. As a result, the amount of thermal dimensional change in the film can be reduced, and gas barrier properties can be greatly improved. Here, the propylene/ethylene copolymer is preferably one in which 1 to 7% by weight of ethylene is randomly copolymerized with propylene, and the ethylene/propylene/butene copolymer is preferably one in which propylene is randomly copolymerized with 1 to 5% by weight of ethylene. , butene is preferably copolymerized in an amount of 3 to 20% by weight. Lamination thickness is not particularly limited, but may be 1 to 8 μm,
From the viewpoint of gas barrier properties and dimensional stability, the thickness is preferably 1 to 3.5 μm. Next, an example of the method for producing the polypropylene film of the present invention will be explained. The extruder temperature is 210-280℃, the isotactic index is more than 90%, the limit [η] 1.2-2.5
Melt dl/g of polypropylene resin and extrude it into a sheet through a T-die with slits.
It is cooled and solidified using a cooling roll at ℃ to form an unstretched sheet. At this time, if necessary, a propylene-ethylene copolymer or/and an ethylene-propylene-butene copolymer are melt-extruded from another extruder and laminated using a T-die to form a laminated unstretched sheet. This unstretched sheet is stretched 3 to 6 times in the length direction while heating in an oven heated to 133 to 144°C, and then stretched 7 to 12 times in the width direction at a temperature of 155 to 165°C.
It is stretched twice and heat treated at a temperature of 155 to 165°C while relaxing 8.5 to 12% in the width direction. Thereafter, the film is introduced into a mixed gas of nitrogen and carbon dioxide gas (volume ratio of carbon dioxide gas: 0.5 to 50%), and while maintaining the film temperature at 40 to 100°C, preferably 45 to 90°C, the film is heated at 20 to 120 W. The A side is subjected to corona discharge treatment at a rate of 100% of the film forming speed ratio. Further, the film thus obtained is slit to a predetermined width and length, and it is preferable that the longitudinal tension at the time of slitting is also low. The method of measuring the characteristic value and the method of evaluating the effect of the present invention are as follows. (1) Measuring method of atomic composition ratio of film surface layer Using ESCA750 manufactured by Shimadzu Corporation, the film surface was treated with excitation X-ray: MgK〓 1,2 line, photoelectron escape angle was 90 degrees, C 1s main peak was Adjust the binding energy value to 284.6eV and adjust the 1s axial path.
From the spectrum obtained by ESCA measurement, C 1s
The area ratio between the peak of The ratio of the number of nitrogen atoms/the number of carbon atoms, that is, the value of N/C. (2) Temperature at which heat loss begins in the longitudinal direction of the film (℃) Using a thermomechanical analyzer (TMA system) manufactured by Perkin-Elmer, a sample measuring 14 mm in the length direction and 5 mm in the width direction was taken from the film. After setting the film so that the sample length is 10 mm without wrinkles or tilting, 1 mm 2 (cross-sectional area) of the film is set.
A load of 40 g was applied to each sample, and the temperature of this sample was raised from a heating start temperature of 25°C at a heating rate of 10°C/min.
When a heating dimensional change curve is drawn with the dimensional change rate on the vertical axis and the temperature on the horizontal axis, the temperature at the intersection of the heating dimensional change curve with the dimensional change rate 0% axis (the dimensional change rate increases at the beginning as the temperature increases) The temperature at which the temperature increases, reaches a maximum value, then decreases to 0% again) is defined as the heat recovery start temperature. FIG. 1 is an example of a heating dimensional change curve,
1 is a heating dimensional change curve, and 2 is a heat loss start temperature. (3) Gas barrier properties (A) Water vapor permeability Measured according to JIS Z 208. At this time, it was set so that the evaporation surface was on the calcium chloride side. (B) Oxygen permeability After leaving the film at room temperature and humidity for one week,
Oxygen permeability was measured according to ASTM-D-1434 using an OX-TRAN100 oxygen permeability measuring device manufactured by Modern Controls. (4) Vapor deposition adhesive strength Evaluation was made by the remaining area of metal adhesion after laminating a commercially available cellophane adhesive tape (registered trademark "Cello Tape") to the metal vapor deposition surface and peeling it off at 90°. Remaining area Adhesion index 95% or more 5 90% or more and less than 95% 4 75% or more and less than 90% 3 50% or more and less than 75% 2 Less than 50% Judgment was made according to the criteria of 1. The higher the adhesion index, the better the adhesion. (5) Abrasion resistance of vapor-deposited surfaces Rub the vapor-deposited surfaces together 10 times under a load of 5 g/cm 2 pressure.
Judgment was made as follows based on the difference in gloss before and after rubbing. Glossiness reduction rate (ΔG) = Glossiness before rubbing - Glossiness after 10 rubs / Glossiness before rubbing ○: ΔG≧0.95 △: 0.85≦ΔG<0.95 ×: ΔG<0.85 (6) F5 value Using Tensilon, film width 10mm, sample length
A 100 mm sample was pulled at a tensile speed of 300 mm/min, and the strength (Kg) at 5% elongation of the film was divided by the cross-sectional area (mm 2 ) of the film. [Function] By setting the surface of A side to a specific atomic composition ratio (O/C, N/C), the metal vapor deposition film is not damaged or peeled off due to wear, and the vapor deposition adhesion is strong. becomes. What should be noted here is that if the surface has a specific atomic composition ratio, it will ooze out from the polypropylene surface layer during metal vapor deposition and increase the intermolecular force between the metal microcrystals. The filling state becomes dense, and as a result, it is effective in suppressing gas permeation with extremely few crystal defects and voids. In addition, the temperature at which heat loss begins in the film length direction is set to 105
By setting the temperature above 0.degree. C., changes in shrinkage dimensions of the film due to heat generation during vapor deposition are suppressed, and metal vapor deposition cracks are prevented, thereby improving gas barrier properties. [Example] The present invention will be explained based on an example. Example 1 A propylene homopolymer with an [η] of 2.2 dl/g and an isotactic index of 96.5% was melt-extruded at an extruder temperature of 270°C, cooled and solidified in a cooling drum at 40°C, and an unstretched sheet was obtained. I made it. This sheet was passed through an oven heated to 141°C and stretched 5 times in the longitudinal direction while being heated. Next, this uniaxially stretched film was heated to 115°C and subjected to 3% relaxation. Next, while heating to 163℃,
Stretched 9 times in the width direction and heat treated at 160℃ with 9.5% relaxation in the width direction to a thickness of 20μ
A biaxially oriented polypropylene film of m was prepared.
Next, one side (Side A) of this film was heated to 80°C in a mixed gas of nitrogen and carbon dioxide gas (volume fraction of carbon dioxide gas: 10%), corona discharge treated at 26 W min/ m2 , and rolled. I took it. O/C, N/ of the film
C. The heat loss start temperature was calculated and shown in Table 1. Furthermore, this film was coated with a 1000mm width vapor deposition machine for 300mm
Aluminum was deposited to a thickness of 35 nm on the A side at a rate of m/min. Table 1 shows the properties of the deposited film. Example 2 A propylene homopolymer having an [η] of 1.85 dl/g and an isotactic index of 97.5% was melt-extruded at an extrusion temperature of 260° C. to produce a uniaxially stretched film in the same manner as in Example 1. Next, this uniaxially stretched film was subjected to 4.8% relaxation while being heated at 130°C. Subsequently, the film was stretched 9 times in the width direction while being heated to 164°C, and the rest was carried out in exactly the same manner as in Example 1 to produce a biaxially stretched polypropylene film.
Next, it was heated to 80° C. in a mixed gas of nitrogen and carbon dioxide and subjected to corona discharge treatment at 29 W·min/m 2 . Subsequently, aluminum vapor deposition was performed in the same manner as in Example 1. The film properties are shown in Table 1. Comparative Examples 1 to 3 Biaxially stretched films were made in the same manner as in Example 1, except that the corona discharge treatment strength was changed to provide O/C and N/C as shown in Table 1. Aluminum was deposited in the same way as Matsutaku. The characteristics are shown in Table 1. Comparative Example 4 A biaxially stretched film was prepared in the same manner as in Example 1, and then one side (side A) of this film was heated in air to 65°C and corona discharge treated at 24W min/ m2 . The film was wound up in the same manner as in Example 1, and aluminum was deposited on the A side of the film to a thickness of 35 nm in the same manner as in Example 1. The characteristics are shown in Table 1. Comparative Example 5 A propylene homopolymer with [η] of 2.2 dl/g and isotactic index of 96.5% was melt-extruded at an extrusion temperature of 270°C, cooled and solidified in a cooling drum at 40°C, and an unstretched sheet was produced. Ivy. This sheet was passed through an oven heated to 135°C and stretched 5 times in the longitudinal direction while being heated. Next, this uniaxially stretched film was subjected to 2% relaxation at 110°C, then stretched 9 times in the width direction while being heated to 162°C, and heat treated at 155°C while applying 9.5% relaxation in the width direction. A biaxially stretched polypropylene film with a thickness of 20 μm was produced. The film was subjected to surface treatment and aluminum vapor deposition in the same manner as in Example 1. The film properties are shown in Table 1. Example 3 A propylene homopolymer with [η] 1.85 dl/g and an isostatic index of 97.5% was melt-extruded from one extruder at an extrusion temperature of 260°C, while an ethylene homopolymer was melt-extruded from another extruder. A propylene random copolymer (ethylene content 3.7% by weight) was melt extruded and laminated with a die. The thickness of the biaxially stretched film at this time was 16.5 μm for the polypropylene layer and 3.5 μm for the propylene/ethylene copolymer layer. Then, in the same manner as in Example 1, biaxial stretching, surface corona treatment, and aluminum vapor deposition were performed. The properties of the obtained film are shown in Table 1. As is clear from Table 1, Examples 1, 2, and 3
It can be seen that the film of the present invention has strong metal deposition adhesion, wear resistance, and excellent gas barrier properties (water vapor permeability, oxygen permeability). On the other hand, in Comparative Examples 1 to 4, if the atomic ratio of the surface layer is not within a specific range, the vapor deposition adhesive strength and the abrasion resistance of the vapor deposited film are poor, and the gas barrier properties are also poor. Furthermore, in Comparative Example 5, the gas barrier properties became poor as the heat recovery start temperature became lower.

〔発明の効果〕〔Effect of the invention〕

本発明は、上述したように、ポリプロピレンフ
イルムの表面の原子構成比を特定化し、かつ、フ
イルム長手方向の熱収開始温度を特定化したこと
により、次のごとき優れた効果が得られた。 (1) 金属蒸着接着性に優れたフイルムとすること
ができた。 (2) 金属蒸着後の気体遮断性に優れたフイルムと
することができた。
As described above, the present invention provides the following excellent effects by specifying the atomic composition ratio on the surface of the polypropylene film and specifying the temperature at which heat loss begins in the longitudinal direction of the film. (1) A film with excellent adhesion to metal vapor deposition could be obtained. (2) A film with excellent gas barrier properties after metal vapor deposition could be obtained.

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

第1図は、熱収開始温度を測定する際に得られ
る加熱寸法変化曲線の一例である。
FIG. 1 is an example of a heating dimensional change curve obtained when measuring the heat loss start temperature.

Claims (1)

【特許請求の範囲】 1 ポリプロピレンフイルムの片面の表層の原子
構成比(酸素原子の数/炭素原子の数)が0.10〜
0.34、(窒素原子の数/炭素原子の数)が0.005〜
0.08の範囲にあり、かつ、該フイルムの長さ方向
の熱収開始温度が105℃以上であることを特徴と
する蒸着用ポリプロピレンフイルム。 2 該片面の反対側面にプロピレン・エチレン共
重合体またはエチレン・プロピレン・ブテン共重
合体を積層したことを特徴とする請求項1記載の
蒸着用ポリプロピレンフイルム。
[Claims] 1. The atomic composition ratio (number of oxygen atoms/number of carbon atoms) of the surface layer on one side of the polypropylene film is 0.10 to 0.10.
0.34, (number of nitrogen atoms/number of carbon atoms) is 0.005~
0.08, and a heat loss onset temperature in the longitudinal direction of the film is 105° C. or higher. 2. The polypropylene film for vapor deposition according to claim 1, wherein a propylene/ethylene copolymer or an ethylene/propylene/butene copolymer is laminated on the opposite side of the one side.
JP25602889A 1989-09-27 1989-09-27 Metallizable polypropylene film Granted JPH03115329A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP25602889A JPH03115329A (en) 1989-09-27 1989-09-27 Metallizable polypropylene film

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP25602889A JPH03115329A (en) 1989-09-27 1989-09-27 Metallizable polypropylene film

Publications (2)

Publication Number Publication Date
JPH03115329A JPH03115329A (en) 1991-05-16
JPH0571613B2 true JPH0571613B2 (en) 1993-10-07

Family

ID=17286915

Family Applications (1)

Application Number Title Priority Date Filing Date
JP25602889A Granted JPH03115329A (en) 1989-09-27 1989-09-27 Metallizable polypropylene film

Country Status (1)

Country Link
JP (1) JPH03115329A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002036354A (en) * 2000-05-16 2002-02-05 Gunze Ltd Easily adhesive polyolefinic biaxially stretched film and method for manufacturing the same
JP2003082137A (en) * 2001-09-10 2003-03-19 Gunze Ltd Laminated film and architectural building material containing the same

Also Published As

Publication number Publication date
JPH03115329A (en) 1991-05-16

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