CN113120296A - 气浮式薄膜贴合设备及其气浮滚轮 - Google Patents

气浮式薄膜贴合设备及其气浮滚轮 Download PDF

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CN113120296A
CN113120296A CN202011327047.0A CN202011327047A CN113120296A CN 113120296 A CN113120296 A CN 113120296A CN 202011327047 A CN202011327047 A CN 202011327047A CN 113120296 A CN113120296 A CN 113120296A
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air
film
roller
floating
laminating
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CN113120296B (zh
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杨思枬
王清和
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Huineng Holding Co ltd
Prologium Technology Co Ltd
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Huineng Holding Co ltd
Prologium Technology Co Ltd
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  • Engineering & Computer Science (AREA)
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Abstract

本发明涉及一种气浮式薄膜贴合设备及其气浮滚轮,通过特定角度能吹出气流的气浮滚轮所构成,而能适用于具有立体障碍的基膜,通过气流提供的正压来填补因立体障碍所产生的空间缺陷,使其能够与贴合膜紧密贴合,克服因立体障碍所产生的皱折、缺陷以及所衍生无法将膜面贴合平整的缺失。

Description

气浮式薄膜贴合设备及其气浮滚轮
技术领域
本发明是有关于一种薄膜贴合设备,特别是一种通过气浮滚轮的气流来填补待贴合薄膜上的缺陷空间,克服因立体障碍所产生的皱折、缺陷以及所衍生无法将膜面贴合平整的缺失的气浮式薄膜贴合设备及其气浮滚轮。
背景技术
近年来,各种电子产品朝向轻薄、微小化发展,使得各种薄膜贴合技术的应用层面更为广泛,最常见的薄膜贴合技术为滚轮卷绕(roll to roll)的方式,其为一种高效能、连续性的生产方式,专门处理可挠性质的薄膜贴合加工,利用待贴合的筒状原料与欲贴合的薄膜筒状原料,以滚轮带动压合的方式来进行连续性的贴合,贴合完成后可再卷成圆筒状或进行裁切,以作为半成品供后续加工使用。
薄膜贴合的主要关键在于如何使薄膜贴合后不产生皱折,使贴合后的积层体能够平整,前案譬如WO2011093427A1号的PCT专利,主要利用绝缘性薄膜、金属箔、间隔薄膜、金属箔、以及绝缘性薄膜重叠并进行热压合,再从间隔薄膜剥离而获得两个单面积层体,使其能够贴合平整。
然而,于待贴合薄膜的背面具有涂层的情况下,涂层会形成立体障碍,立体障碍之间会产生空间缺陷,再加上薄膜的厚度较薄,无法提供足够的挺性,贴合时就会产生皱折、缺陷的情况,使其贴膜非常不平整;然现有技术上,尽管提出许多改善贴合平整的技术,但却并未考虑具有立体障碍的情况。
有鉴于此,本发明提出一种崭新的气浮式薄膜贴合设备及其气浮滚轮,以解决上述具有立体障碍的贴膜所面临的问题。
发明内容
本发明的主要目的在于提供一种气浮式薄膜贴合设备及其气浮滚轮,可解决上述现有技术的缺失,可利用气浮滚轮于滚动压合的过程中持续提供正压的气流,来填补待贴合薄膜的立体障碍间的空间缺陷,以达到贴合的平整性。
为达到上述目的,本发明提供一种气浮式薄膜贴合设备及其气浮滚轮,其包含有至少二个进料滚轮、贴合滚轮以及气浮滚轮,进料滚轮可以导引基膜与贴合膜来进行贴合,其中基膜具有第一表面以及对应的第二表面,且第二表面上具有至少二个片状薄膜组件,于该些片状薄膜组件间形成缺陷空间,贴合滚轮可接受进料滚轮所导引的贴合膜,配合气浮滚轮可接受进料滚轮所导引的基膜,且气浮滚轮设置并紧邻于贴合滚轮的对应位置,而可通过贴合滚轮的压合,将贴合膜贴合至基膜的第一表面;于贴合过程中,气浮滚轮可持续提供正压的气流至基膜的第二表面,可以填补于缺陷空间,增加基膜的挺性而能使其与贴合膜平整地贴合。
另一方面,气浮滚轮包含有外滚轮、内轮与一进气源,外滚轮可相对内轮转动,且其外表面具有多个吹气孔,内轮为固定不转动且设置于外滚轮内,其外表面于预定角度范围具有多个通孔,可接收进气源的气流,通过内轮的通孔与外滚轮的吹气孔,而可于贴合过程中将气流填补于基膜的缺陷空间,且其中预定角度范围约为20-90度;如此一来,即可克服因立体障碍所产生的皱折、缺陷以及所衍生无法将膜面贴合平整的缺失。
底下通过具体实施例详加说明,当更容易了解本发明的目的、技术内容、特点及其所达成的功效。
附图说明
图1A为本发明的实施例所提供的气浮滚轮的示意图。
图1B为本发明的实施例所提供的气浮滚轮的分解示意图。
图2A、2B为本发明的实施例所提供的气浮滚轮的使用状态示意图。
图3为本发明的实施例所提供的气浮式薄膜贴合设备示意图。
图4为本发明的实施例所提供的气浮式薄膜贴合设备的压和剖面示意图。
附图标记
10 气浮滚轮
11 外滚轮
111 吹气孔
12 内轮
121 通孔
21 贴合滚轮
31 第一进料滚轮
32 第二进料滚轮
33 自由轮
34 收料滚轮
40 基膜
401 第一表面
402 第二表面
41 片状薄膜组件
50 贴合膜
L 中心线
θ 预定角度
具体实施方式
本发明所公开的一种气浮滚轮,其可于贴合过程中持续提供正压的气流,来填补待贴合薄膜上的缺陷空间,使其不产生皱折、缺陷而能确实平整地贴合;请参阅图1A、1B,气浮滚轮10包含有外滚轮11与内轮12,外滚轮11可相对转动以配合带动待贴合薄膜来进行压合,因此,外滚轮11概略为中空圆筒状,其外表面具有多个吹气孔111,因外滚轮11直接接触于待贴合薄膜,因此吹气孔111的部份尺寸不宜太大,此部份容后详述。而内轮12为固定不转动且设置于外滚轮11内,其外表面于预定角度范围具有多个通孔121,因为内轮12无需配合待贴合薄膜或贴合过程中来转动,仅需能导引进气源来通过通孔121,因此,内轮12可为部份实心或空心皆可,仅需能将气流导引至通孔121即可,而相较于前述的外滚轮11的吹气孔111,通孔121的尺寸可以较大,来提供足够的气流。
为了说明其气流导引与通孔121配置的角度,请接续参阅图2A、2B,气浮滚轮10可配合贴合滚轮21来针对待贴合的基膜40与贴合膜50来进行压合贴合,基膜40具有相对的第一表面401以及第二表面402,贴合膜50贴合于基膜40的第一表面401,而基膜40的第二表面402上具有多个片状薄膜组件41,因此,基膜40上的片状薄膜组件41因具有一定的厚度则会形成立体障碍,而立体障碍之间则会形成空间缺陷,因此,当进行贴合时,基膜40的第二表面402上的空间缺陷则会影响基膜40与贴合膜50之间的贴合度。
由于片状薄膜组件41的厚度非常薄,且片状薄膜组件41易于碎裂,因而非常难以直接应力压合来使其平整贴合,因此本发明的气浮滚轮10可提供正压的气流,概略来说,其压力可为0.1-0.3kg/cm2,并配合气浮滚轮10的内轮12与外滚轮11的设计,而可于贴合过程中持续提供气流来填补于基膜40的第二表面402上的空间缺陷,增加基膜40的挺性,使其能于平整状态下与贴合膜50来进行贴合,因此,提供气流的预定角度θ,其范围概略为20-90度,其计算基准为概略由气浮滚轮10的中心轴至基膜40与贴合膜50接触点为中心线L,沿着此中心线L两侧计算的角度,原则上,两侧的角度可大致上相同,举例来说,当预定角度θ为90度时,则可配置中心线L两侧各为45度角的范围;当然,根据不同的贴合状况,此配置也可为两侧不相等的状况,譬如考虑空间缺陷较难填补(譬如范围较大或是形状较复杂等),则可设计贴合前的吹气角度(图中左侧)较大、或是当基膜40与贴合膜50较难贴合(譬如材质问题),则可设计贴合后的吹气角度(图中右侧)较大。
接着请同时配合图1A-2B,因此,为了达到前述吹气效果,气浮滚轮10的外滚轮11的外表面可为满布吹气孔111,以确保外滚轮11于贴合过程中不论转动到任何角度,气流皆可导引出来,如前所述,吹气孔111的尺寸不宜过大,以确保外滚轮11与基膜40的贴合度;而内轮12的部分,则为预定角度θ的范围分布有通孔121,原则上通孔121的尺寸也不宜过大,以确保气流导引的均匀性,但整体而言,通孔121的尺寸可大于吹气孔111。
请参阅图3,为本发明的实施例所提供的气浮式薄膜贴合设备示意图,气浮式薄膜贴合设备包含有至少两个进料滚轮、贴合滚轮21与气浮滚轮10,进料滚轮的数量可根据贴合薄膜的数量而定,如图中所绘示,包含有第一进料滚轮31与第二进料滚轮32,第一进料滚轮31用以导引贴合膜50,而第二进料滚轮32用以导引基膜40,当然,如为更多膜层相互贴合,则会设置对应数量的进料滚轮,此处说明仅为配合图式说明,并非用以限制其数量与位置。
以下举一实际实施态样来做说明,贴合膜50可为PET(聚对苯二甲酸乙二酯)或其他塑料薄膜,而基膜40可为譬如铜、铝等金属薄膜,其厚度概略为0.006-0.02毫米(mm),而其上具有特殊图样的涂层(片状薄膜组件41),厚度可为0.1-0.3毫米,涂层可以是通过无机粉末混合作为黏着剂的高分子所形成,因此,涂层是非常易碎的。基膜40与贴合膜50分别通过第一进料滚轮31与第二进料滚轮32的导引,来分别通过贴合滚轮21与气浮滚轮10所接收,而气浮滚轮10设置紧邻于贴合滚轮21,来使贴合膜50与基膜40相互贴合;同时更可配合自由轮33的设置来调整基膜40的进料角度。
贴合滚轮21的硬度可控制为40-90度(萧氏硬度),来避免硬度过高或过低所产生薄膜积层不易贴合或是破裂的情况,此外,由于片状薄膜组件41厚度非常小且非常易碎,难以直接压合于基膜40的第二表面402来进行贴合,因此,本发明于贴合过程中通过气流提供的正压来填补第二表面402的片状薄膜组件41间的空隙。请参阅图4,气浮滚轮10的内轮12接收进气源的气流,并导引使其通过内轮12的通孔121与外滚轮11的吹气孔111,来填补于基膜40的片状薄膜组件41之间的空间缺陷,增加基膜40的挺性,使其能平整地与贴合膜50贴合,而不产生皱折、缺陷。贴合完成后,再通过收料滚轮34予以将贴合后的薄膜积层卷绕收纳;当然,亦可配合其他设备或装置,直接进行连续加工。
以上所述,仅为本发明的较佳实施例而已,并非用来限定本发明实施的范围。故即凡依本发明权利要求所述的特征及精神所为的均等变化或修饰,均应包括于本发明的权利要求范围内。

Claims (10)

1.一种气浮式薄膜贴合设备,该气浮式薄膜贴合设备包含有:
至少二个进料滚轮,可以导引一基膜与一贴合膜来进行贴合,其中该基膜具有一第一表面以及对应的一第二表面,且该第二表面上具有至少二个片状薄膜组件,该些片状薄膜组件间形成一缺陷空间;
一贴合滚轮,接受该进料滚轮所导引的该贴合膜;以及
一气浮滚轮,接受另一该进料滚轮所导引的该基膜,且设置并紧邻于该贴合滚轮的对应位置,而可通过该贴合滚轮的压合,将该贴合膜贴合至该基膜的该第一表面,其中该气浮滚轮包含有:
一外滚轮,其外表面具有多个吹气孔,并可相对转动;
一内轮,设置于该外滚轮内,其外表面于一预定角度范围具有多个通孔;以及
一进气源,连接该内轮,以注入一气流至该内轮,通过该内轮的该通孔与该外滚轮的该吹气孔,而于该预定角度范围内将该气流填补于该基膜的该第二表面的该缺陷空间;
其中该预定角度范围为20-90度。
2.根据权利要求1所述的气浮式薄膜贴合设备,其中该基膜为一金属薄膜。
3.根据权利要求2所述的气浮式薄膜贴合设备,其中该金属薄膜的厚度为0.006-0.02毫米。
4.根据权利要求1所述的气浮式薄膜贴合设备,其中该进气源的该气流的压力为0.1-0.3kg/cm2
5.根据权利要求1所述的气浮式薄膜贴合设备,其中该基膜的该片状薄膜组件的厚度为0.1-0.3毫米。
6.根据权利要求1所述的气浮式薄膜贴合设备,其中该贴合滚轮的表面硬度为40-90度(萧氏硬度)。
7.根据权利要求1所述的气浮式薄膜贴合设备,其中该通孔的尺寸大于该吹气孔。
8.一种气浮滚轮,用于配合一贴合滚轮而将一基膜与一贴合膜来进行贴合,其中该基膜具有一第一表面以及对应的一第二表面,且该第二表面上具有至少二个片状薄膜组件,该些片状薄膜组件间形成一缺陷空间,该气浮滚轮包含有:
一外滚轮,其外表面具有多个吹气孔,并可相对转动;
一内轮,设置于该外滚轮内,其外表面于一预定角度范围具有多个通孔;以及
一进气源,连接该内轮,以注入一气流至该内轮,通过该内轮的该通孔与该外滚轮的该吹气孔,而于该预定角度范围内将该气流填补于该基膜的该第二表面的该缺陷空间;
其中该预定角度范围为20-90度。
9.根据权利要求8所述的气浮滚轮,其中该进气源的该气流的压力为0.1-0.3kg/cm2
10.根据权利要求8所述的气浮滚轮,其中该通孔的尺寸大于该吹气孔。
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