TW200814892A - Manufacturing method of flexible laminated plate - Google Patents

Manufacturing method of flexible laminated plate Download PDF

Info

Publication number
TW200814892A
TW200814892A TW096110936A TW96110936A TW200814892A TW 200814892 A TW200814892 A TW 200814892A TW 096110936 A TW096110936 A TW 096110936A TW 96110936 A TW96110936 A TW 96110936A TW 200814892 A TW200814892 A TW 200814892A
Authority
TW
Taiwan
Prior art keywords
layer
thermal expansion
resin
polyimide
expansion coefficient
Prior art date
Application number
TW096110936A
Other languages
Chinese (zh)
Other versions
TWI392427B (en
Inventor
Tomoyuki Suzuki
Masahiko Takeuchi
Original Assignee
Nippon Steel Chemical Co
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 Nippon Steel Chemical Co filed Critical Nippon Steel Chemical Co
Publication of TW200814892A publication Critical patent/TW200814892A/en
Application granted granted Critical
Publication of TWI392427B publication Critical patent/TWI392427B/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/06Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/04Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/28Layered products comprising a layer of synthetic resin comprising synthetic resins not wholly covered by any one of the sub-groups B32B27/30 - B32B27/42
    • B32B27/281Layered products comprising a layer of synthetic resin comprising synthetic resins not wholly covered by any one of the sub-groups B32B27/30 - B32B27/42 comprising polyimides
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/24Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with at least one layer not being coherent before laminating, e.g. made up from granular material sprinkled onto a substrate
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09DCOATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
    • C09D179/00Coating compositions based on macromolecular compounds obtained by reactions forming in the main chain of the macromolecule a linkage containing nitrogen, with or without oxygen, or carbon only, not provided for in groups C09D161/00 - C09D177/00
    • C09D179/04Polycondensates having nitrogen-containing heterocyclic rings in the main chain; Polyhydrazides; Polyamide acids or similar polyimide precursors
    • C09D179/08Polyimides; Polyester-imides; Polyamide-imides; Polyamide acids or similar polyimide precursors
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K1/00Printed circuits
    • H05K1/02Details
    • H05K1/03Use of materials for the substrate
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/24Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with at least one layer not being coherent before laminating, e.g. made up from granular material sprinkled onto a substrate
    • B32B2037/243Coating

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Materials Engineering (AREA)
  • Wood Science & Technology (AREA)
  • Organic Chemistry (AREA)
  • Laminated Bodies (AREA)

Abstract

Provided is a manufacturing method of flexible laminated plate, wherein a required processing time of a heating step after dispensing a polyimide precursor resin solution on a conductive metal foil is short, so as to provide a flexible laminated plate having a low extension elasticity modulus, an excellent flexibility, and an excellent dimension stability. According to the manufacturing method of flexible laminated plate of the present invention, a polyimide precursor resin solution is dispensed on a conductive metal foil, and the polyimide precursor resin solution is then dried and cured by a heating processing, wherein, a total heating time of not less than 90 DEG C; in the heating processing is in a range of 5-25 minutes; the ratio of a heating time of 90-200 DEG C; to a heating time of more than 200 DEG C is set to be 9:1-7:3; the extension elasticity modulus of the polyimide resin layer formed on the conductive metal foil is controlled to be 3-6 Gpa,and the coefficient of heat expansion is controlled to be in a range of 16-28 ppm/DEG C.

Description

1 200814892 -九、發明說明: -【發明所屬之技術領域】 本發明係關於一種在金屬箔上設置由聚醯亞胺樹脂構 成之絕緣層的撓性積層板之製造方法。 【先前技術】 撓性積層板係由金屬層與絕緣層構成,因為具有可於 性,因而使用於要求柔軟性與彎曲性的部分之配線基板二 對電子機器的小型化、輕量化具有貢獻。即使在挽^積層 板中,絕緣層亦使用聚醯亞胺樹脂者,由於耐熱性與尺; 穩定性佳,因而廣泛使用於行動電話、資訊終端機等的配 f基板。製造撓性積層板的方法,係有如:利用環氧樹脂 專黏合劑將聚醯亞胺樹脂薄膜貼合在金屬落而進行梦造的 方法,或者在金屬箔上直接塗佈聚醯亞胺樹脂或其先㈣ 脂溶液而進行製造的方法。特別係由後者方法所與得者, 不會有因黏合劑所造成的特性降低之情形,而成為活用聚 w胺糸樹脂特性的撓性積層板。(例如參照專利文獻 近年來,可攜式電子機H的小型化、輕量化正日益發 折=須在機器内的非常狹窄空間中將配線基板: 料折亚安裝。所以,對挽性積層板 、彎折。提升撓性積層板彎折性的方土 士1 谷易 此口 蚵注的方法,有如將金屬箔或絕 、、、削薄、或降低絕緣層的拉伸彈性率等方法。其卜 :降低有效使用為絕緣層的聚酸亞胺樹脂之拉伸彈性^1 200814892 - IX. Description of the Invention: - Technical Field to Which the Invention Is A The present invention relates to a method for producing a flexible laminate comprising an insulating layer made of a polyimide resin on a metal foil. [Prior Art] The flexible laminated board is composed of a metal layer and an insulating layer, and has flexibility, and thus contributes to downsizing and weight reduction of a wiring board used in a portion requiring flexibility and flexibility. Even in the laminated board, the insulating layer is made of a polyimide resin, and it is widely used in a f-substrate such as a mobile phone or an information terminal because of its heat resistance and ruler stability. The method for manufacturing a flexible laminate is, for example, a method in which a polyimide resin film is bonded to a metal by an epoxy resin-specific adhesive, or a polyimide resin is directly coated on a metal foil. Or a method of manufacturing the first (iv) fat solution. In particular, the latter method is obtained, and there is no such a problem that the characteristics caused by the binder are lowered, and it becomes a flexible laminate which utilizes the properties of the poly-amine resin. (For example, in the recent years, the miniaturization and weight reduction of the portable electronic device H are becoming increasingly folded. The wiring substrate is required to be mounted in a very narrow space in the machine. Therefore, the laminated laminate is required. Bending, which is a method of improving the bending property of a flexible laminated board, such as a metal foil or a thinner, or a lowering of the tensile modulus of the insulating layer.卜: Reducing the tensile elasticity of the polyimide resin which is effectively used as an insulating layer ^

二==在聚醯亞胺的分子主鏈中,導入可彎曲的:鍵 甲基鍵結等。例如將以[4,-氧化二苯胺⑽A 319059 6 200814892 ” oxydiani 1 ine)為原料單體的一種聚醯亞胺先質樹脂進行 ,合成,藉由將其醯亞胺化,俾可獲得拉伸彈性率較低的产 醯亞胺樹脂絕緣層(例如參照專利文獻2、3、4)。Two == In the molecular backbone of the polyimine, a bendable bond: a methyl bond or the like is introduced. For example, a polyiminoimine precursor resin using [4,-diphenylamine (10) A 319059 6 200814892 "oxydiani 1 ine" as a raw material monomer is synthesized and synthesized by yttrium yttrium. A ytterbium imide resin insulating layer having a low modulus of elasticity (see, for example, Patent Documents 2, 3, and 4).

然而’就該等專利文獻所記載的聚酿亞胺樹脂之單芦 薄膜而言,當在金屬落上施行塗佈或積層而形成二生 板時,難以在聚醯亞胺與金屬層間將獲得充分的黏合強s 度。解決上述問題的方法係將聚醯亞胺樹脂層予以多層 化、,並在鄰接金屬荡之侧設置與金屬箔具良好黏合二二熱 可塑性聚ϋ亞胺系樹脂層,並在該熱可塑性翻亞胺樹脂 層的外侧(與金屬側相反之侧),形成彈性 ^ 亞胺系樹脂層之手法。 - [專利文獻丨]曰本專利第3034838號公報 [專利文獻2]日本特開2003-109989號公報 [專利文獻3]日本特開2003-192788號公報 [專利文獻4]日本專利第3523952號公 _ 【發明内容】 (發明所欲解決之課題) 層予二二:吏用熱可塑性聚酿亞胺樹脂而將絕緣 數變大,㈣性言會發生絕緣層整體的熱膨脹係 持可承受作為撓寸穩定性惡化之情形。為了維 將樹脂溶液塗用時的充分尺寸穩以生,必須 降低的問題。 理時間拉長’而將導致生產性 本發明係為了 解决忒項問題而經深入鑽研的結果,其 319059 7 200814892 在於提供—種撓性積層板,其於撓性積層板的製造步 ^ ,將聚酿亞胺先質樹脂溶液塗饰於導電性金屬落上= 、加熱步驟所需要的處理時間短,且拉 低^ : 性佳、尺寸穩定性佳。 低$折 (解決課題之手段) 明者等為了解決上述課題,經深入鑽研的結果發 取利用㈣法進行之撓性積層板之製造方法中 =亞胺先質樹脂溶液塗佈後的加熱處理步驟設定為特 ^太/尸可控制絕緣層的特性,而完成本發明。換句話 樹受明的撓性積層板之製造方法,係將聚醯亞胺先質 醮=液f布於導電性金屬落上,並藉由加熱處理而使聚 二胺先貝树脂溶液乾燥且硬化的撓性積層板之製造方 鬥二其特徵為,於加熱處理中,將9〇〇c以上的合計加熱時 ⑶分的範圍’並將在9代以上且2〇代以下的 力=時間、與在超過20代溫度下的加熱時間之比例設定 抖t· 1至7: 3 ’且將形成於導電性金屬荡上的聚酸亞胺 ^曰層之拉㈣㈣控制為3至6GPa,並將熱膨脹係數控 在16至28ppm/°C範圍内。 (發明之效果) 根據本發明,此夠以較短的加熱處理時間製造彎折性 2寸穩定性佳的撓性積層板,且具有提高具有此種優越 知〖生之撓性積層板的生產性之效果。 【實施方式】 以下,針對本發明進行詳細說明。 319059 8 200814892 、一本發明所製造的撓性積層板係在導電性金屬荡(以下 /簡稱「金屬箔」)上具有聚醯亞胺樹脂層。而且,在金屬箔 上形成聚醯亞胺樹脂層之方法係依下述方式進行,即在金 ’屬荡上塗佈聚醯亞胺先質樹脂溶液,再施行乾燥、硬化的 加熱處理,藉此將上述聚醯亞胺先質轉換成聚酿亞胺。而 且,所製造之撓性積層板的聚醯亞胺樹脂層之拉伸彈性率 為3至6GPa’熱恥脹係數在Μ至28ppm/cc範圍内。另外, _本發明中所謂的「聚酸亞胺樹脂」係指由例如聚酿亞胺、 聚醯胺醯亞胺、聚醚醯亞胺、聚矽氧烷醯亞胺等,在分子 構造中具有醯亞胺基的聚合物所構成的樹脂。 本發明所使用的導電性金屬箔,係可列舉例如以銅、 銘、不錢鋼、鐵、銀、妃、鎳、銘、鉻、錮、鶴、或該等 的合金為構成元素的金屬箔。金屬箔中,最好為銅箔或合 金銅箔。金屬箔的厚度最好在5至35//m範圍内,尤以9 至18//m範圍内為佳。若金屬箔比35//111厚,則積層板將 •變硬,導致彎曲性、f折性變差。若金屬箔比薄,則 在積層板的製造步驟中,難以進行張力等的調整,導致容 易發生皺折等不良狀況。此外,該等金屬箔係在提升黏合 力專目的下’亦可對其表面施以化學性或機械性表面處理。 本發明所使用的聚醯亞胺先質樹脂溶液係可依照周知 方法進行製造。例如使四羧酸二酐與二胺化合物溶解於大 致等莫耳有機溶劑中,並在〇至l〇〇°c中施行30分鐘至24 小時的攪拌,進行反應而獲得者。有關聚合時所使用的有 機溶劑,係可列舉例如:N,N一二曱基曱醯胺、N,N-二甲基 9 319059 .200814892 ,乙醯胺、N—甲基—N 一吡咯啶酮、二甲亞砜、硫酸二甲酯、酚、 -齒化酚、環己酮、二噚烷、四氫呋喃、二甘醇二甲醚、三 甘醇二甲醚等。亦可合併使用2種以上之上述化合物。聚 醯亞胺先質樹脂溶液的黏度最好在5〇〇cp至looooocp範圍 内。若超過該範圍,則當利用塗佈機等施行塗佈作業時容 易在薄膜上發生厚度不均、條紋等不良狀況。 有關所使用的四羧酸二酐與二胺化合物,係可配合本 發明之撓性積層板的聚醯亞胺樹脂層特性,適當地選擇使 用上述化合物中之1種或2種以上。本發明中,必須將聚 醯亞胺樹脂層的拉伸彈性率設定在3至6GPa範圍内,且將 熱膨脹係數設定在16至28Ppm/°C範圍内,而為了使在形 成撓性積層板時金屬箔與聚醯亞胺樹脂層間之黏合性呈良 好狀態,最好將聚醯亞胺樹脂層形成為複數層。 當將聚醯亞胺樹脂層形成複數層時,鄰接金屬箔的 層,最好設定為熱膨脹係數為3〇ppm/t以上的高熱膨脹係 數聚酿亞胺樹脂層。就高熱膨脹係數聚醯亞胺樹脂層而 言,最好具有一般式(1)所示之構造單位。However, in the case of the mono-ruthenium film of the polyacrylonitrile resin described in the patent documents, when the coating is deposited or laminated on the metal to form a dicot, it is difficult to obtain between the polyimide and the metal layer. Full adhesion to strong s degrees. The method for solving the above problem is to multilayer the polyimine resin layer, and to provide a good adhesion of the second thermoplastic resin polyimide layer to the metal foil on the side adjacent to the metal slant, and to turn the thermoplastic in the thermoplastic The outer side of the imide resin layer (the side opposite to the metal side) forms a method of forming an elastic amine-based resin layer. - [Patent Document No. 3] Japanese Patent Laid-Open No. Hei. No. 2003-192788 (Patent Document 3) Japanese Patent Publication No. 2003-192788 (Patent Document 4) Japanese Patent No. 3523952 _ [Summary of the Invention] (Problems to be solved by the invention) Layer 2: The use of thermoplastic polyacrylamide resin to increase the number of insulation, (4) The thermal expansion of the entire insulating layer can be sustained as a scratch The situation in which the stability of the inch deteriorates. In order to maintain a sufficient size when the resin solution is applied, it is necessary to reduce the problem. The time is elongated and will lead to productivity. The present invention has been thoroughly studied in order to solve the problem. The 319059 7 200814892 is to provide a flexible laminate which is manufactured in a flexible laminate. The polyaniline precursor resin solution is coated on the conductive metal drop =, the processing time required for the heating step is short, and the pull-down is good: good property and good dimensional stability. In the method of manufacturing a flexible laminated board by the method of (4), the heat treatment after the application of the imine precursor resin solution is carried out in order to solve the above problems. The steps are set to specifically control the characteristics of the insulating layer to complete the present invention. In other words, the method for manufacturing a flexible laminated board is characterized in that the polyimine precursor 醮 = liquid f is placed on the conductive metal, and the polydiamine kebab resin solution is dried by heat treatment. And the manufacturing of the hardened flexible laminated board is characterized in that, in the heat treatment, the total range of 9 〇〇c or more is heated (the range of 3 minutes) and the force of 9 generations or more and 2 generations or less = The ratio of the time to the heating time at a temperature of more than 20 generations is set to t·1 to 7:3′ and the pull (4) (4) of the polyacid imide layer formed on the conductive metal swash is controlled to 3 to 6 GPa. The coefficient of thermal expansion is controlled in the range of 16 to 28 ppm / ° C. (Effects of the Invention) According to the present invention, it is possible to manufacture a flexible laminate having excellent bending stability of 2 inches with a short heat treatment time, and to improve the production of a flexible laminate having such superiority. The effect of sex. [Embodiment] Hereinafter, the present invention will be described in detail. 319059 8 200814892 A flexible laminate produced by the present invention has a polyimide resin layer on a conductive metal slab (hereinafter referred to as "metal foil"). Further, the method of forming a polyimide layer on a metal foil is carried out by coating a polyimide resin precursor solution on a gold stalk and then performing a drying and hardening heat treatment. This converts the above polyimine precursor into a brewin. Further, the polyimide laminate layer of the manufactured flexible laminate has a tensile modulus of 3 to 6 GPa' and a coefficient of thermal contraction in the range of Μ to 28 ppm/cc. In addition, the term "polyimide resin" as used in the present invention means, for example, a polyacrylimine, a polyamidimide, a polyether quinone, a polydecane ylide, or the like, in a molecular structure. A resin composed of a polymer having a quinone imine group. The conductive metal foil used in the present invention is, for example, a metal foil containing copper, melamine, iron, silver, silver, iridium, nickel, chrome, niobium, crane, or an alloy thereof. . Among the metal foils, copper foil or alloy copper foil is preferred. The thickness of the metal foil is preferably in the range of 5 to 35 / / m, particularly preferably in the range of 9 to 18 / / m. If the metal foil is thicker than 35//111, the laminate will become harder, resulting in deterioration of bendability and f-folding. When the ratio of the metal foil is thin, it is difficult to adjust the tension or the like in the manufacturing step of the laminated board, and it is easy to cause wrinkles and the like. In addition, the metal foils may be subjected to a chemical or mechanical surface treatment on the surface for the purpose of improving the adhesion. The polybendylene precursor resin solution used in the present invention can be produced by a known method. For example, the tetracarboxylic dianhydride and the diamine compound are dissolved in a general molar organic solvent, and stirred for 30 minutes to 24 hours in 〇 to 10 ° C to obtain a reaction. The organic solvent used in the polymerization may, for example, be N,N-didecylguanamine, N,N-dimethyl 9 319059 . 200814892 , acetamidine, N-methyl-N-pyrrolidine Ketone, dimethyl sulfoxide, dimethyl sulfate, phenol, - dentated phenol, cyclohexanone, dioxane, tetrahydrofuran, diglyme, triethylene glycol dimethyl ether and the like. Two or more of the above compounds may also be used in combination. The viscosity of the polyimine precursor resin solution is preferably in the range of 5 〇〇 cp to looooocp. When it exceeds this range, when a coating operation is performed by a coater or the like, it is easy to cause defects such as thickness unevenness and streaking on the film. The tetracarboxylic dianhydride and the diamine compound to be used may be one or more selected from the above-mentioned compounds, as appropriate, in combination with the properties of the polyimine resin layer of the flexible laminate of the present invention. In the present invention, it is necessary to set the tensile modulus of the polyimide film to a range of 3 to 6 GPa, and to set the coefficient of thermal expansion in the range of 16 to 28 Ppm/° C., in order to form a flexible laminate. The adhesion between the metal foil and the polyimide layer is in a good state, and it is preferable to form the polyimide layer into a plurality of layers. When the polyimine resin layer is formed into a plurality of layers, the layer adjacent to the metal foil is preferably set to a high thermal expansion coefficient polyamidene resin layer having a thermal expansion coefficient of 3 〇ppm/t or more. In the case of a high thermal expansion coefficient polyimine resin layer, it is preferred to have a structural unit represented by the general formula (1).

式中,匕係從下述構造式(2)與(3)所示之基中選擇之 至> 1種的基,R2係從下述(4)與(5)所示基中選擇之至少 1種的基。此外,下述構造式(4)中,χ係指-s〇2—、—c〇— 及直接鍵結中之任一者。 319059 10 (3) (2) 200814892 χ>πχ ⑷ XX (5) 當將聚酿亞胺樹脂層形成為複數層時,最好 高熱膨脹健《亞胺樹脂層的㈣(與金屬^相反: :Γ:::彈,率為4至8GPa的基底聚酿亞胺樹脂層。 土底_亞㈣脂層最好具有—般式(6)所示之構造單位:In the formula, the lanthanoid series is selected from the groups shown by the following structural formulas (2) and (3) to a group of >, and R2 is selected from the groups shown by the following (4) and (5). At least one type of base. Further, in the following structural formula (4), the hydrazone refers to any of -s〇2—, —c〇— and a direct bond. 319059 10 (3) (2) 200814892 χ>πχ (4) XX (5) When the layer of the polyimide resin layer is formed into a plurality of layers, it is preferable to thermally expand the "imide resin layer (4) (in contrast to the metal ^:: Γ::: The base of the base polyimide resin layer with a ratio of 4 to 8 GPa. The soil layer _ sub (four) grease layer preferably has the structural unit shown by the general formula (6):

(6) 式中,R3 係-CH3、-C2Hs、_〇CH3、一〇C2H5 中任一取代基。 最好R3係-CHs。此外,戎φ,γ τ,八〆 飞中X y刀別係指構成單位的構 成比率^係設定在〇·4^0·6範圍内3係設定在〇·6 至0· 4粑圍内,且X + y=1。χ與y的比例中,若X小於〇·[ 則聚醯亞胺樹脂的熱膨脹係數會變大,而有在形成挽性積 層板㈣尺寸穩定性降低,且積層板容易發生捲曲的傾 向。反之,若X大於〇·6,則聚醯亞胺的拉伸彈性率會變 大,而有形成撓性積層板時之彎折性降低的傾向。(6) wherein R3 is any one of -CH3, -C2Hs, _〇CH3, or 〇C2H5. The best R3 is -CHs. In addition, 戎φ, γ τ, and the 〆 中 X X 系 系 系 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ 4 4 4 4 4 3 3 3 3 3 3 3 3 3 3 3 3 3 And X + y=1. In the ratio of χ to y, if X is less than 〇·[the thermal expansion coefficient of the polyimine resin becomes large, the dimensional stability of the laminated laminate (4) is lowered, and the laminate tends to be curled. On the other hand, when X is more than 〇6, the tensile modulus of the polyimine will increase, and the bendability at the time of forming the flexible laminate tends to be lowered.

、,聚酿亞胺樹脂層形成為複數料,撓性積層板的層 構k最好構成為在金m設置高熱膨脹係數聚 醯亞胺樹 月曰層,亚在其上面依序積層基底聚醯亞胺樹脂層的構造。 更么的層構造係金屬箔/高熱膨脹係數聚醯亞胺樹脂層/基 底承醯亞胺樹脂層/咼熱膨脹係數聚醯亞胺樹脂層。如此, 11 319059 .200814892 8當製作在聚醯亞胺樹脂層之單側具有金屬箔的單面撓性積 /層板之後,再將金屬箱加熱壓接於於樹脂面侧、較佳為高 熱膨服係數聚酸亞胺樹脂層上,藉此亦可製作在聚醯亞S 樹脂層雙面具有金屬箔的雙面撓性積層板。 本發明係採取在金屬箱上施行聚酿亞胺先質樹脂溶液 的塗佈,並進行加熱處理的製造方法,但必須將在該製造 步驟中之乾燥與硬化步驟中,9(rc以上的合計加熱時間設 定為谷至25分鐘。其中,若合計加熱時間比5分鐘短,聚 醯亞胺樹脂將容易發生發泡等不良狀況。反之,若合計加 熱時間超過25分鐘,則撓性積層板的生產性將惡化。此 外,必須將乾燥與硬化步驟中的合計加熱時間中、阶以 上且20(TC以下的加熱時間、與在超過2〇〇t:溫度下的加執 時間之比例設定為9: 1至7: 3。若在9代以上且低於· /C的溫度下之加熱時間比例未達合計加熱時間的·,則 有聚酿亞胺層的熱膨脹係數變大、或撓性積層板的尺寸穩 _定性降低、或積層板捲曲的情形發生。反之,若低於_ °c溫度下的加熱時間比例超過合計加熱時間的9⑽,則當 在超過20(TC溫度下施行加熱處理時,升溫速度過大,導 致聚醯亞胺容易發生發泡等不良狀況。另外,當聚酿亞胺 樹脂層係由複數層構成時,則合計對在各層所塗佈的聚酸 ^胺先質樹脂溶液施以乾燥之時間,更加計使該等硬化的 時間,而求取加熱時間。此外,有關超過2〇〇它的加熱溫 度,因為聚醯亞胺樹脂層開始劣化,因❿最好將加熱溫度 之上限設定為450°C。 319059 12 .200814892 : 撓性積層板的聚醯亞胺樹脂層之厚度,最好設定在5 •至40 # m範圍内。尤以8至35 # m為佳。若聚醯亞胺樹脂 層的厚度比5 # m薄,則當作絕緣層時的強度較脆弱,在對 挽性積^板施行加工時,容易導致薄膜發生破裂等狀況。 反之,右厚度比40//m厚,則薄膜較不易彎折,造成撓性 ,層板的、3折性降低。當將聚醯亞胺樹脂層設為複數層 ^基底㈣亞胺樹脂層與高鱗關數㈣亞胺樹脂層 ,佳比率,係以各自的合計厚度為基準,基底聚酿亞胺 树脂層/高熱膨脹係數聚醢亞胺樹脂層為i至4〇,更佳 至 30。 . ^明的撓性積層板之製造方法中,聚醯亞胺樹脂層 ㈣i生率必須设定為3至6GPa,同時,必須將熱膨脹 數,…6至28卿气。聚酸亞胺樹脂層的拉伸彈性 則ι車Γ仏1&圍係3.5至5.5GPa。若拉伸彈性率低於3Gpa, 、進行撓性積層板之加工時難以處理,反之,若高於 孰廢性積層板的彎折性會降低。聚醯亞胺樹脂層的 的 佳細系17至2W。。。若聚酿亞靡^ 之差值超過該範圍,則因為與銅箔的熱膨脹係數間 板會發生捲曲。為了將c寸交化會變大’且積層 為了將來鉍亞胺樹脂層的拉伸彈性率與埶 恥脹係數控制於上述範 千/、”'、 脂層的構成單位者,“擇輪構成《亞胺樹 佳地進㈣二 述加熱處理條件,即可效率 進仃撓〖生積層板的製造。 (實施例) 319059 13 200814892 • 以下’利用實施例更詳細地說明本發明。此外,實施 /例中所使用的縮寫,係如下述: DMAC · N,N-二甲基乙醯胺 m-TB : 2, 2’ ~二甲基一4, 4’ -二胺基聯苯 0M : 44’ -二胺基二苯醚 BAPP = 2,2’-雙(4-胺基苯氧基苯基)丙烷 PMDA :均苯四甲酸酐 ⑩ 阶1)八:3,3’-4,4’-聯苯基四羧酸二酐 實施例中,聚醯亞胺樹脂層的拉伸彈性率與熱膨脹係 數之評估係依以下方法實施。 拉伸彈性率:使用東洋精機(股)製Strograph® R-1進 行測量。(根據 IPC-TM-650, 2. 4. 19) 熱%脹係數:使用Seiko Instruments(股)製熱分析裝 置TMA-1〇〇,升溫至255t^^,在該溫度下保持1Q分鐘後, 再依5°C /分的速度進行冷卻,求出從24〇°c至i〇〇°c的平 籲均熱膨脹率(熱膨脹係數)。、 [合成例1] 將m-TB(6當量)及〇DA(4當量)在室溫下施行攪拌而溶 解在可拆式燒瓶中之DMAc。接著,添加PMDA(9 86當量)。 然後,繼續攪拌約3小時而進行聚合反應,獲得聚醯亞胺 先質樹脂溶液a。此外,DMAc係使用m—ΤΒ、0M及PMDA 的裝填濃度為16重量%的量。將所調製得聚醯亞胺先質樹 脂溶液a,在銅箔(Nikko Materials股份有限公司製鋼箔 BHY-22B-T、厚度:18/zm。以下簡稱為「銅箔」時係指該銅 319059 14 :200814892 4)上均勻塗佈成26〇A m厚度,並在125。匸下施行3分鐘 •的加熱乾魅’而將溶劑予以去除。然後,在⑽。C至綱 °C溫度範圍内施行8分3〇秒,在2〇11至3赃溫度範圍 =施行j分30秒的加熱處理,而進行醯亞胺化反應,而獲 侍在銅伯上形成有厚約28 # m聚醯亞胺層的積層體。利用 钱刻處理去除該積層體的銅落層,而獲得聚酿亞胺薄膜。 經測量所獲得之聚醯亞胺薄膜的拉伸彈性率與熱膨脹係 數,結果分別為 6. 8GPa、12. 6ppm/°c。 [合成例2 ] 除m-TB係使用5當量、0DA係使用5當量之外,其餘 勻依舨與合成例1相同的方法施行聚合反應,而獲得聚醯 亞胺先質樹脂溶液b。使用所調製之聚醯亞胺先質樹脂溶 液b,依照與合成例1相同的方法獲得聚醯亞胺薄膜,經 測量拉伸彈性率與熱膨脹係數,結果分別為5· 9GPa、 17· lppm/°C。 •[合成例3 ] 除m-TB係使用4當量、ODA係使用6當量之外,其餘 均依照與合成例1相同的方法施行聚合反應,而獲得聚酿 亞胺先質樹脂溶液c。使用所調製之聚醯亞胺先質樹脂溶 液c ’依照與合成例1相同的方法獲得聚醯亞胺薄膜,經 測量拉伸彈性率與熱膨脹係數,結果分別為5. 1GPa、 23· lppm/〇C。 [合成例4] 除m-TB係使用1 〇當量、〇DA係使用0當量之外,其 319059 15 200814892 f 餘均依照與合成例1相同的方法祐 > 取人e — 乃套知仃聚合反應,而獲得聚 :醯亞胺先質樹脂溶液d。使用所,制 文用所凋製之聚醯亞胺先質樹脂 溶液d,依照與合成例i相同的方法獲得聚酿亞胺薄膜, 經測量拉伸彈性率與熱膨脹係數,結果分別為13鳥、 -5· lppm/〇C 〇 [合成例5] 除m-TB係使用〇當量、〇DA係使用1〇當量之外,其 •餘均依照與合成们相同的方法施行聚合反應,而獲得聚 酸亞胺先質樹脂溶液e。使用所調製之聚醒亞胺先質樹脂 溶液e,依照與合成例丨相同的方法獲得聚醯亞胺薄膜, 經測量拉伸彈性率與熱膨脹係數,結果分別為2.7〇ρ&、 43· 4ppm/°C。 [合成例6 ] 將BAPPU0當量)在室溫下施行攪拌而溶解在可拆式 燒瓶中之DMAc。接著,添加pMDA(9.69當量)與BpDA(〇.5l ⑩當量)。然後,繼續攪拌約3小時而進行聚合反應,而獲得 聚S&亞胺先質樹脂溶液f。此外,dmIc係使用RAPP、PMDA 及BPM的裝填浪度為12重量%的量。除使用所調製之聚醯 亞先貝树脂〉谷液f塗佈成厚度3 5 0 // m之外,其餘均依照 與合成例1的相同方法,獲得厚約28//m的聚醯亞胺薄膜, 經測量拉伸彈性率與熱膨脹係數,結果分別為2. 6GPa、 50· Tppm/^C。 [實施例1] 在銅箔上,將依合成例6所調製之聚醯亞胺先質樹脂 319059 16 200814892 i溶液f均勻地塗佈成50// m厚度,並在i25°C下施行加熱 /乾爍而將溶劑予以去除。接著,以積層於其上面的方式, 將依合成例1所調製之聚醯亞胺先質樹脂溶液3均勻地塗 佈成190//m厚度,並在125°C下施行加熱乾燥。並且在其 上面’再度將聚醯亞胺先質樹脂溶液f均勻地塗佈成5〇 #爪 厚度,並在125°C下施行加熱乾燥。截至此為止的加熱乾 燥時間合計係設定為3分鐘。然後,在13 〇它至2 〇 〇 溫度 ⑩範圍内施行8分30秒的加熱處理,在2〇rc至36〇它溫^ 範圍内施行3分30秒的加熱處理,而進行醯亞胺化反應"; 而獲彳于在銅、冶上开》成厚約2 8 // m聚酿亞胺層的積層體。利 用蝕刻處理去除該積層體的銅箔層,而獲得聚醯亞胺薄 膜。經測罝所獲得之聚醯亞胺薄膜的拉伸彈性率與熱膨脹 係數’結果如表1所示。 [實施例2] 除取代聚醯亞胺先質樹脂溶液a,改為使用溶液b之 馨外,其餘均依照與實施μ相同的方法獲得聚醯亞胺薄 膜,並測量拉伸彈性率與熱膨脹係數。結果如表丨所示。 [實施例3 ] 除取代聚酿亞胺先質樹脂溶液&,改為使用溶液c之 1 ’其餘均依照與實施例1相同的方法獲得聚醯亞胺薄 膜,並測量拉伸彈性率與熱膨脹係數。結果如表丨所示。 [比較例1 ] 除取代聚醯亞胺先質樹脂溶液a,改為使用溶液d之 外’其餘均依照與實施例1相同的方法獲得聚醯亞胺薄 319059 17 200814892 膜,並測量拉伸彈性率與熱膨脹係數。結果如表〗所示。 ^ [比較例2] ’ 除取代聚醯亞胺先質樹脂溶液a,改為使用溶液e之 外,其餘均依照與實施例1相同的方法獲得聚醯亞胺薄 膜,並測量拉伸彈性率與熱膨脹係數。結果如表1所示。 [比較例3] ’、 至聚醯亞胺先質樹脂溶液的塗佈、加熱乾燥(〗25、3 ❿分鐘)為止均依照與實施例i相同的方法實施。然後,在 13(TC至200°C溫度範圍内施行6分鐘的加熱處理,在2〇ι t至360°C溫度範圍内施行6分鐘的加熱處理,並進行醯 亞胺化反應,而獲得在銅箔上形成厚約28 Am聚醯亞胺層 的積層體。利用蝕刻處理去除該積層體的銅箔層,而獲得 聚醯亞胺薄膜。經測量所獲得之聚醯亞胺薄膜的拉伸彈性 率與熱膨脹係數,結果如表1所示。The poly-imine resin layer is formed into a plurality of materials, and the layer structure k of the flexible laminate is preferably configured to set a high thermal expansion coefficient of the polyimine tree in the gold m, and sub-layers are sequentially stacked thereon. The structure of the quinone imine resin layer. Further, the layer structure is a metal foil/high thermal expansion coefficient polyimine resin layer/base yttrium imide resin layer/咼 thermal expansion coefficient polyimine resin layer. Thus, 11 319059 . 200814892 8 After making a single-sided flexible product/layer having a metal foil on one side of the polyimide layer, the metal box is heat-bonded to the resin side, preferably high heat. On the polyacetimimine resin layer, the double-coated flexible laminate having a metal foil on both sides of the polyimide resin layer can be produced. The present invention adopts a production method in which a coating of a polyaniline precursor resin solution is carried out on a metal case and heat treatment is performed, but in the drying and hardening steps in the production step, 9 (the total of rc or more is required) The heating time is set to the valley for 25 minutes, and if the total heating time is shorter than 5 minutes, the polyimine resin is likely to cause problems such as foaming. Conversely, if the total heating time exceeds 25 minutes, the flexible laminate is The productivity is deteriorated. In addition, it is necessary to set the ratio of the heating time in the drying and hardening steps to the order of 9 or more and the heating time of 20 or less and the addition time of more than 2〇〇t: the temperature to 9 : 1 to 7: 3. If the heating time ratio at the temperature of 9 or more and lower than /C is less than the total heating time, the thermal expansion coefficient of the polyimine layer becomes large, or the flexible laminate The dimensional stability of the plate is reduced, or the laminate is curled. Conversely, if the heating time ratio below the temperature of _ °c exceeds 9 (10) of the total heating time, when the heat treatment is performed at more than 20 (TC temperature) ,Rise When the temperature is too high, the polyimine is likely to cause problems such as foaming. Further, when the polyimino resin layer is composed of a plurality of layers, the polyacid precursor precursor resin solution applied to each layer is added in total. The drying time is applied, and the hardening time is taken into account, and the heating time is determined. In addition, regarding the heating temperature of more than 2 Torr, since the polyimide layer begins to deteriorate, it is preferable to heat the temperature. The upper limit is set to 450 ° C. 319059 12 .200814892 : The thickness of the polyimide layer of the flexible laminate is preferably set in the range of 5 • to 40 # m, particularly preferably 8 to 35 # m. When the thickness of the polyimide layer is less than 5 #m, the strength when used as an insulating layer is weak, and when the processing is performed on the sheet, the film is likely to be broken or the like. 40 / / m thick, the film is less likely to bend, resulting in flexibility, laminate, 3 fold reduction. When the polyimine resin layer is set to multiple layers ^ substrate (four) imine resin layer and high scale (4) The imine resin layer, the good ratio is based on the total thickness of each The base polyimine resin layer/high thermal expansion coefficient polyimine resin layer is from i to 4 Å, more preferably 30%. In the manufacturing method of the flexible laminated board, the polyimide layer (i) yield Must be set to 3 to 6 GPa, at the same time, the number of thermal expansions must be ..., 6 to 28 qing. The tensile elasticity of the polyimide resin layer is ι Γ仏 1 & the range is 3.5 to 5.5 GPa. The rate is lower than 3 Gpa, and it is difficult to handle the processing of the flexible laminated board. On the contrary, if the bending property is higher than that of the depleted laminated board, the fineness of the polyimide layer is 17 to 2 W. If the difference between the 酿 靡 靡 超过 超过 超过 超过 超过 , , , , , , , , , , , 超过 超过 超过 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜 铜The elastic modulus and the 埶 胀 系数 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制 控制The manufacture of laminates. (Embodiment) 319059 13 200814892 • Hereinafter, the present invention will be described in more detail by way of examples. In addition, the abbreviations used in the examples/examples are as follows: DMAC · N,N-dimethylacetamide m-TB : 2, 2' ~ dimethyl-4,4'-diaminobiphenyl 0M : 44'-diaminodiphenyl ether BAPP = 2,2'-bis(4-aminophenoxyphenyl)propane PMDA: pyromellitic anhydride 10 steps 1) 8: 3, 3'-4 In the example of 4'-biphenyltetracarboxylic dianhydride, the evaluation of the tensile modulus of elasticity and the coefficient of thermal expansion of the polyimide layer of the polyimide resin was carried out in the following manner. Tensile modulus: The measurement was carried out using a Strograph® R-1 manufactured by Toyo Seiki Co., Ltd. (According to IPC-TM-650, 2. 4. 19) Thermal % expansion coefficient: using a Seiko Instruments thermal analyzer TMA-1, heating up to 255 t^^, after holding at this temperature for 1Q minutes, Further, cooling was carried out at a rate of 5 ° C /min, and the mean thermal expansion coefficient (thermal expansion coefficient) from 24 ° C to i 〇〇 ° c was determined. [Synthesis Example 1] m-TB (6 equivalents) and hydrazine DA (4 equivalents) were stirred at room temperature to dissolve DMAc in a separable flask. Next, PMDA (9 86 equivalents) was added. Then, stirring was continued for about 3 hours to carry out a polymerization reaction to obtain a polyamidene precursor resin solution a. Further, DMAc uses an amount of loading of m-ΤΒ, 0M, and PMDA of 16% by weight. The polyiphthalide precursor resin solution a prepared in the copper foil (the steel foil BHY-22B-T made by Nikko Materials Co., Ltd., thickness: 18/zm. Hereinafter referred to as "copper foil") means the copper 319059 14:200814892 4) Evenly coated to a thickness of 26 〇A m and at 125. The solvent is removed by applying the heat for 3 minutes. Then, at (10). C to the °C temperature range of 8 minutes and 3 seconds, in the temperature range of 2〇11 to 3赃 = j minutes and 30 seconds of heat treatment, and the hydrazine imidization reaction, and the formation on the copper There is a layered body with a thickness of about 28 # m polyimine layer. The copper falling layer of the laminate is removed by a solvent treatment to obtain a polyimide film. The tensile elastic modulus and thermal expansion coefficient of the polyimide film obtained by the measurement were 6.8 GPa and 12.6 ppm/°c, respectively. [Synthesis Example 2] A polymerization reaction was carried out in the same manner as in Synthesis Example 1 except that 5 equivalents of the m-TB system and 5 equivalents of the 0DA system were used, and a polybine imine resin solution b was obtained. Using the prepared polyimine precursor resin solution b, a polyimide film was obtained in the same manner as in Synthesis Example 1, and the tensile modulus and the coefficient of thermal expansion were measured, and the results were 5. 9 GPa, 17·1 ppm/ °C. [Synthesis Example 3] The polymerization reaction was carried out in the same manner as in Synthesis Example 1 except that 4 equivalents of the m-TB system and 6 equivalents of the ODA system were used, and the polyaniline precursor resin solution c was obtained. GPa, 23·lppm/, respectively, the tensile modulus and thermal expansion coefficient were measured, respectively, and the results were 5. 1 GPa, 23·1 ppm/, respectively, using a polyetherimine precursor resin solution c'. 〇C. [Synthesis Example 4] Except that the m-TB system used 1 〇 equivalent and the 〇DA system used 0 equivalent, the 319059 15 200814892 f remainder was in the same manner as in Synthesis Example 1 and was taken as a person. The polymerization was carried out to obtain a poly(indenine) precursor resin solution d. In the same manner as in the synthesis example i, the polyimide film was obtained by the same method as in the synthesis example i, and the tensile modulus and the coefficient of thermal expansion were measured, and the results were 13 birds, respectively. -5·lppm/〇C 〇 [Synthesis Example 5] Except that m-TB is used in the equivalent of 〇, and 〇DA is used in the same amount, the remainder is obtained by the same method as the synthesis. Polyacid imine precursor resin solution e. Using the prepared polyamidamine precursor resin solution e, a polyimide film was obtained in the same manner as in the synthesis example, and the tensile modulus and the coefficient of thermal expansion were measured, and the results were 2.7 〇 ρ & 4.4 ppm, respectively. /°C. [Synthesis Example 6] DMAc was dissolved in a separable flask by stirring BAPPU0 equivalent) at room temperature. Next, pMDA (9.69 equivalents) and BpDA (〇.5l 10 equivalents) were added. Then, the polymerization was carried out by further stirring for about 3 hours to obtain a poly-S&imine precursor resin solution f. Further, dmIc uses an amount of loading of 12% by weight of RAPP, PMDA and BPM. A polythene layer having a thickness of about 28//m was obtained in the same manner as in Synthesis Example 1, except that the prepared polyfluorene resin was used to coat the thickness of 3,500 Å. The average tensile strength and thermal expansion coefficient were 2. 6 GPa, 50 · Tppm / ^ C, respectively. [Example 1] On a copper foil, a solution of the polyimine precursor resin 319059 16 200814892 i prepared according to Synthesis Example 6 was uniformly coated to a thickness of 50 / / m, and heated at i25 ° C / Drying to remove the solvent. Next, the polyimine precursor resin solution 3 prepared in accordance with Synthesis Example 1 was uniformly coated to a thickness of 190 / / m in a manner of being laminated thereon, and dried by heating at 125 ° C. Further, on the top, the polyiminoimine precursor resin solution f was uniformly applied to a thickness of 5 〇 #爪, and heat-dried at 125 °C. The total heating drying time up to this point was set to 3 minutes. Then, it is subjected to heat treatment for 8 minutes and 30 seconds in the range of 13 至 to 2 〇〇, and heat treatment is performed for 3 minutes and 30 seconds in the range of 2 〇 rc to 36 〇, and yttrium imidization is performed. The reaction "; and won the thick layer of about 2 8 // m poly-imine layer in the copper and metallurgy. The copper foil layer of the laminate was removed by an etching treatment to obtain a polyimide film. The results of tensile modulus and coefficient of thermal expansion of the polyimide film obtained by the measurement of yttrium are shown in Table 1. [Example 2] A polyimide film was obtained in the same manner as in the practice of μ except that the polyethylenimine precursor resin solution a was used instead of the solution b, and the tensile modulus and thermal expansion were measured. coefficient. The results are shown in the table. [Example 3] A polyimine film was obtained in the same manner as in Example 1 except that the substituted polyanilin precursor resin solution & was used instead of the solution c, and the tensile modulus and the tensile modulus were measured. Thermal expansion coefficient. The results are shown in the table. [Comparative Example 1] A film of polytheneimide thin 319059 17 200814892 was obtained in the same manner as in Example 1 except that the substituted polyimine precursor resin solution a was used instead of the solution d, and the tensile was measured. Elasticity and coefficient of thermal expansion. The results are shown in the table. ^ [Comparative Example 2] 'A polyimide film was obtained in the same manner as in Example 1 except that the polyethylenimine precursor resin solution a was replaced, and the solution e was used instead, and the tensile modulus was measured. With coefficient of thermal expansion. The results are shown in Table 1. [Comparative Example 3] The procedure was carried out in the same manner as in Example i until the application of the polyimine precursor resin solution and the heating and drying (25 minutes, 3 minutes). Then, heat treatment is carried out for 6 minutes in a temperature range of 13 (TC to 200 ° C, heat treatment is carried out for 6 minutes in a temperature range of 2 〇 to 360 ° C, and hydrazine imidization reaction is carried out to obtain A laminate of about 28 Am polyimine layer is formed on the copper foil. The copper foil layer of the laminate is removed by etching to obtain a polyimide film. The stretch of the polyimide film obtained by measurement is obtained. Elasticity and coefficient of thermal expansion, the results are shown in Table 1.

[表1][Table 1]

319059 18319059 18

Claims (1)

200814892 V ^ 十、申請專利範園: • 1. 一觀性積層板之製造方法,係藉由將㈣亞胺先 腊溶液塗佈於導電性金Μ上,並藉由加熱處理而使聚 醯亞胺先質樹脂溶液乾燥且硬化的挽性積層板之製造 方法’其特徵為,在加熱處理中,將9(rc以上的合計 加熱時間設為5至25分的範圍,並將在9〇〇c以上且_ c以下的加熱時間、與在超過2〇〇它溫度下的加熱時間 鲁之比例設定為9:丨至7: 3,且將形成於導電性金屬謂 亡的聚醯亞胺樹脂層之拉伸彈性率控制為3至6GPa, 亚將熱膨脹係數控制在16至28ppm/t:2範圍。 如申明專利範圍第1項之撓性積層板之製造方法,其 中聚醯亞胺樹脂層的厚度係在5至4〇 "之範圍,且 由複數層構成,並具有至少一層的熱膨脹係數為 PPm/ C以上的尚熱膨脹係數聚醯亞胺樹脂層、及至少 一層的拉伸彈性率為4至8GPa的其基底聚醯亞胺樹脂 層,且鄰接導電性金屬箔的層係高熱膨脹係數 樹脂層。 319059 19 % 200814892 ” 七、指定代表圖:無 ^ (一)本案指定代表圖為:第()圖。 (二)本代表圖之元件符號簡單說明: • 八、本案若有化學式時,請揭示最能顯示發明特徵的化學式: 本案無代表之化學式。200814892 V ^ X. Application for Patent Park: • 1. A method for manufacturing an observational laminate by applying (iv) an imine prior wax solution to a conductive metal crucible and heating it to make it agglomerated A method for producing a leaching laminated plate in which an imine precursor resin solution is dried and hardened is characterized in that, in the heat treatment, a total heating time of 9 (rc or more is set to a range of 5 to 25 minutes, and will be at 9 〇. The ratio of the heating time above 〇c and below _c to the heating time in the temperature above 2 〇〇 is set to 9: 丨 to 7:3, and will be formed on the conductive metal. The tensile modulus of the resin layer is controlled to be 3 to 6 GPa, and the thermal expansion coefficient is controlled to be in the range of 16 to 28 ppm/t: 2. The method for producing a flexible laminate according to the first aspect of the invention, wherein the polyimide resin The thickness of the layer is in the range of 5 to 4 〇" and consists of a plurality of layers, and has at least one layer of thermal expansion coefficient polyimine resin layer having a thermal expansion coefficient of PPm/C or more, and at least one layer of tensile elasticity a layer of a base polyimide layer of 4 to 8 GPa, The layer adjacent to the conductive metal foil is a high thermal expansion coefficient resin layer. 319059 19 % 200814892 ” VII. Designated representative figure: None ^ (1) The representative figure of the case is: () picture. (2) The symbol of the representative figure Brief Description: • 8. If there is a chemical formula in this case, please disclose the chemical formula that best shows the characteristics of the invention: The chemical formula that is not represented in this case. 5 3190595 319059
TW096110936A 2006-03-31 2007-03-29 Manufacturing method of flexible laminated plate TWI392427B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2006098246A JP4593509B2 (en) 2006-03-31 2006-03-31 Method for producing flexible laminate

Publications (2)

Publication Number Publication Date
TW200814892A true TW200814892A (en) 2008-03-16
TWI392427B TWI392427B (en) 2013-04-01

Family

ID=38672178

Family Applications (1)

Application Number Title Priority Date Filing Date
TW096110936A TWI392427B (en) 2006-03-31 2007-03-29 Manufacturing method of flexible laminated plate

Country Status (3)

Country Link
JP (1) JP4593509B2 (en)
KR (1) KR101366043B1 (en)
TW (1) TWI392427B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6031396B2 (en) * 2013-03-29 2016-11-24 新日鉄住金化学株式会社 Manufacturing method of double-sided flexible metal-clad laminate
KR20180069790A (en) * 2015-10-15 2018-06-25 신닛테츠 수미킨 가가쿠 가부시키가이샤 Polyimide laminate and manufacturing method thereof

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0563322A (en) * 1984-01-27 1993-03-12 Hitachi Ltd Manufacture of flexible printed board
JPH0753801B2 (en) * 1986-12-25 1995-06-07 住友ベークライト株式会社 Method for manufacturing flexible printed circuit board
JPH03145185A (en) * 1989-10-31 1991-06-20 Sumitomo Bakelite Co Ltd Flexible printed circuit board
JP4200376B2 (en) 2004-02-17 2008-12-24 信越化学工業株式会社 Flexible metal foil polyimide laminate and method for producing the same
KR100590719B1 (en) * 2004-03-05 2006-06-19 주식회사 엘지화학 The Method of Making 2-Layer Copper Clad Laminate
WO2005087480A1 (en) * 2004-03-15 2005-09-22 Kaneka Corporation Novel polyimide film and use thereof

Also Published As

Publication number Publication date
KR20070098720A (en) 2007-10-05
JP2007268892A (en) 2007-10-18
TWI392427B (en) 2013-04-01
KR101366043B1 (en) 2014-02-21
JP4593509B2 (en) 2010-12-08

Similar Documents

Publication Publication Date Title
TWI777950B (en) Polyimide, polyimide-based adhesive, film-like adhesive material, adhesive layer, adhesive sheet, copper foil with resin, copper-clad laminate and printed wiring board, and multilayer wiring board and method for producing the same
TWI292740B (en) Metallic laminate and method for preparing thereof
TWI321974B (en) Copper clad laminate for chip on film
US9725565B2 (en) Flexible metal laminate and preparation method of the same
TWI500501B (en) Second layer double sided flexible metal laminated board and manufacturing method thereof
JP2016194055A (en) Adhesive composition, film-like adhesive material, adhesive layer, adhesive sheet, copper foil with resin, copper-clad laminate, flexible copper-clad laminate, printed circuit board, flexible printed circuit board, multilayer wiring board, printed circuit board, and flexible printed circuit board
TWI494214B (en) Flexible metal-clad laminate and a method of manufacturing the same
TW200930565A (en) Metal-clad laminate
TWI394659B (en) Method for making high anti-flexion flexible copper clad laminate board
JP2012176619A (en) Laminated body for thermally-conductive flexible board, and thermally-conductive polyimide film
TW201014878A (en) Polyimide precursor and its composition and polyimide laminate
JP2007059892A (en) Manufacturing method for high-flexible copper clad laminate
TW201900392A (en) Roll of laminated film, method for producing the same, and manufacturing method of flexible device
TW200806100A (en) Double side conductor laminates and its manufacture
TWI380744B (en)
TWI249563B (en) Novel polyimide copolymer and metal laminate comprising the same
TW200819000A (en) Laminate for wiring board
JP4426774B2 (en) Thermosetting resin composition, laminated body using the same, and circuit board
TW201226446A (en) A polyimide precursor resin solution
US7384683B2 (en) Substrate for flexible printed wiring board and method for manufacturing the same
TW200814892A (en) Manufacturing method of flexible laminated plate
TWI660649B (en) Flexible circuit board and electronic equipment
TW201251535A (en) Metal-covered laminate board
TW201720858A (en) Polyimide polymer, polyimide film, and flexible copper-coated laminate
JP4936729B2 (en) Flexible printed wiring board substrate and manufacturing method thereof