JPH0453714A - Manufacture of laminated sheet - Google Patents
Manufacture of laminated sheetInfo
- Publication number
- JPH0453714A JPH0453714A JP2164815A JP16481590A JPH0453714A JP H0453714 A JPH0453714 A JP H0453714A JP 2164815 A JP2164815 A JP 2164815A JP 16481590 A JP16481590 A JP 16481590A JP H0453714 A JPH0453714 A JP H0453714A
- Authority
- JP
- Japan
- Prior art keywords
- pressure
- laminated sheet
- structural body
- twisting
- glass transition
- 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.)
- Pending
Links
- 238000004519 manufacturing process Methods 0.000 title claims description 6
- 230000009477 glass transition Effects 0.000 claims abstract description 8
- 229920005989 resin Polymers 0.000 claims abstract description 8
- 239000011347 resin Substances 0.000 claims abstract description 8
- 239000000463 material Substances 0.000 claims abstract description 7
- 238000001035 drying Methods 0.000 claims abstract description 4
- 239000000835 fiber Substances 0.000 claims description 6
- 239000011888 foil Substances 0.000 claims description 3
- 229910052751 metal Inorganic materials 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims description 3
- 238000000465 moulding Methods 0.000 claims description 3
- 229920001187 thermosetting polymer Polymers 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 7
- 238000010438 heat treatment Methods 0.000 abstract description 6
- 239000011521 glass Substances 0.000 abstract description 3
- 229910001220 stainless steel Inorganic materials 0.000 abstract description 3
- 239000010935 stainless steel Substances 0.000 abstract description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 abstract description 2
- 238000002845 discoloration Methods 0.000 abstract description 2
- 239000003822 epoxy resin Substances 0.000 abstract description 2
- 239000004744 fabric Substances 0.000 abstract description 2
- 229920000647 polyepoxide Polymers 0.000 abstract description 2
- 239000002966 varnish Substances 0.000 abstract description 2
- 239000011889 copper foil Substances 0.000 abstract 1
- 230000000052 comparative effect Effects 0.000 description 5
- 238000000137 annealing Methods 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 229920000742 Cotton Polymers 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 239000005062 Polybutadiene Substances 0.000 description 1
- 239000004372 Polyvinyl alcohol Substances 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000012790 adhesive layer Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000010425 asbestos Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- -1 etc. Polymers 0.000 description 1
- 239000010410 layer Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000004745 nonwoven fabric Substances 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 229920002857 polybutadiene Polymers 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920001721 polyimide Polymers 0.000 description 1
- 239000009719 polyimide resin Substances 0.000 description 1
- 229920002451 polyvinyl alcohol Polymers 0.000 description 1
- 229910052895 riebeckite Inorganic materials 0.000 description 1
- 238000002791 soaking Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000012209 synthetic fiber Substances 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
- 229920006337 unsaturated polyester resin Polymers 0.000 description 1
- 239000002759 woven fabric Substances 0.000 description 1
Landscapes
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、プリント配線板Kt’用可能な反り、ねじれ
、1法変化が少ない積層の製造方法に関する0
〔従来の技術〕
従来の積層板は、成形FI8におきる樹脂の流動による
基材の歪み、成るいはステンレス鋼製跳板の線膨張係数
と積層板の線j1張係数との差によって生ずる内部歪が
残留し1反り、ねじれ又は加工工程での寸法変化をおこ
すことが認められる。[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to a method for manufacturing a laminate that can be used for printed wiring boards Kt' and has less warping, twisting, and method changes. [Prior Art] Conventional laminate board In this case, distortion of the base material due to resin flow during molding FI8, or internal distortion caused by the difference between the linear expansion coefficient of the stainless steel spring board and the linear tensile coefficient of the laminate, may remain, resulting in warpage, twisting, or processing. It is recognized that dimensional changes occur during the process.
この問題の対策とし”t・工、積層板をオープン内に積
載して120〜170℃で1時6時間加熱してアニーリ
ング処理をする試みもある。As a countermeasure to this problem, there has been an attempt to stack the laminates in an open space and heat them at 120 to 170° C. for 1 hour and 6 hours to perform an annealing treatment.
上記の対策にも拘らず、積層板の積載体は熱伝導性が悪
いためにアニーリング効果が均等Vc埃われない0又、
オープン内へり積層板の出し入れに伴っておきる異物の
付着、傷及び打痕の発生に免れ難い。Despite the above measures, the stack of laminates has poor thermal conductivity, so the annealing effect is not uniform.
It is inevitable that foreign matter will adhere to the open inner edge, and scratches and dents will occur when the laminate is taken in and out.
本発明は、上記の諸問題にかんがみ1反り、ねじれ又は
寸法変化をおこすこと少な(、かつ異物付層、傷及び打
痕の発生少なき積層板の製造方法を提供することを目的
とする〇
〔課題を解決するための手段〕
上記の目的を達成するために5本発明は、繊維基材に熱
硬化性樹脂を含浸乾燥して得たプリプレグを複数枚重ね
、その外面に金属箔kmね合わせた構成体と鏡板とを交
互に重ねて加熱加圧硬化成形する積層板の製造において
、硬化成形後引続き圧七〇〜20 kg/aIFに下げ
、該硬化物のガラス転位温度より高い温度で一足時間保
持した後冷却することを%徴とする積層板の製造方法で
ある。In view of the above-mentioned problems, an object of the present invention is to provide a method for manufacturing a laminate that causes less warping, twisting, or dimensional changes (and less occurrence of foreign matter layer, scratches, and dents). [Means for Solving the Problems] In order to achieve the above object, the present invention consists of stacking a plurality of prepregs obtained by impregnating and drying a thermosetting resin into a fiber base material, and coating the outer surface with km of metal foil. In the production of a laminate in which the combined structure and mirror plate are stacked alternately and cured under heat and pressure, the pressure is lowered to 70 to 20 kg/aIF after curing, and the temperature is higher than the glass transition temperature of the cured product. This is a method for producing a laminate, which involves holding it for one hour and then cooling it.
本発明の硬化後の圧は、0〜2 o kg/alF、好
ましくは0〜3kg/−とし、その硬化物のガラス転位
温度以上好ましくはガラス転位温度より20〜80℃高
い温度で少なくとも10分以上好ましくは30〜60分
間以上保持する。その後冷却するが、ガラス転位温度以
下、好ましくは30℃以下まで徐冷してプレスから取り
出す0
使用する繊維基材は、紙、綿リンク等の天然櫃維、ポリ
アミド、ポリビニルアルコール、ポリエステル、ポリア
クリル等の曾成繊維及びガラス、アスベスト等の無機線
維の織布、不織布あるいをエマットとする0
熱硬化性樹脂を用い、エポ午シ樹脂、不飽和ポリエステ
ル樹脂、ポリイミド樹脂、ポリブタジェン樹脂等とする
。The pressure after curing of the present invention is 0 to 2 o kg/alF, preferably 0 to 3 kg/-, and the cured product is heated for at least 10 minutes at a temperature higher than the glass transition temperature, preferably 20 to 80 °C higher than the glass transition temperature. It is preferably held for 30 to 60 minutes or longer. After that, it is cooled down to below the glass transition temperature, preferably below 30°C, and then taken out from the press.The fiber base materials used include paper, natural fibers such as cotton links, polyamide, polyvinyl alcohol, polyester, and polyacrylic. Woven fabrics, non-woven fabrics, or emmats are made of synthetic fibers such as glass, asbestos, etc., and thermosetting resins are used, such as epoxy resin, unsaturated polyester resin, polyimide resin, polybutadiene resin, etc. .
金属箔としては、銅、アルはニクム、ニッケル等を用い
うるが、上記本発明条件に対しては%に限定はしない〇
一般に厚さα018〜[LO7O2O3のが好fしく、
必要によって裏面に接着剤層を設ヒる0
〔作用〕
積層板をプレス&1よって加熱加圧成形して冷却した時
、繊維基材及び繊維基材と硬化樹脂との境界部に歪みが
残る。この歪みが積層板の反り、ねじれ及び寸法変化の
原因となる0
本発明は、積層板を加熱加圧して樹脂の硬化反応を完了
した段階で圧七除き力為つガラス転位温度以上の高温に
保持する0この条件によって、残留する歪みの一部が除
かれ1反り、ねじれ及び寸法変化は減少する0
〔実施例〕
次に本発明の詳細な説明する0
(実施例1)
ガラス布基@にエボ中シ樹熊ワニス1kt浸乾燥して得
たプリプレグを所定枚数1ね、さらにその両TIjJV
c厚さ[10351111の鋼陥會真ね合わせた構成体
をステンレス鋼繞板で挾みプレスで加熱加圧成形した。As the metal foil, copper, aluminum, nickel, etc. can be used, but there is no limitation to the percentage according to the conditions of the present invention. In general, the thickness is preferably α018 to [LO7O2O3,
An adhesive layer may be provided on the back side if necessary.0 [Operation] When the laminate is heated and pressure-molded by press&1 and cooled, distortion remains in the fiber base material and the boundary between the fiber base material and the cured resin. This distortion causes warping, twisting, and dimensional changes in the laminate.In the present invention, the laminate is heated and pressurized to complete the curing reaction of the resin, and then the pressure is removed and the laminate is heated to a high temperature above the glass transition temperature. This condition removes some of the residual distortion and reduces warping, twisting, and dimensional changes. [Example] Next, the present invention will be explained in detail. (Example 1) Glass cloth base @ A predetermined number of prepregs obtained by soaking and drying 1kt of Evo medium-sized tree bear varnish, and both TIjJV
A structural body made of steel with a thickness of [10351111] was sandwiched between stainless steel plates and heated and pressed using a press.
すなわち、170℃、60kJl/−で60分間加熱加
圧成形した後、引続いて圧k Okg/ryeとし、温
度170℃で50分間保持し、さらに室温に冷却して厚
さ1Bの積層板を得た。That is, after heating and pressure forming at 170°C and 60kJl/- for 60 minutes, the pressure was increased to kOkg/rye, the temperature was held at 170°C for 50 minutes, and the laminate was further cooled to room temperature to form a 1B thick laminate. Obtained.
(実施例2)
加熱加圧成形に引続いて圧會Okg/aIIとし、温R
170℃で60分間保持した他は、実jIfI例1と同
様托して厚さ1a+sの積層板會得た。(Example 2) Following heating and pressure forming, the pressure was set to Okg/aII, and the temperature was
A laminate plate having a thickness of 1a+s was obtained in the same manner as in Example 1, except that the temperature was maintained at 170°C for 60 minutes.
(比較例1)
実施例1と同様にして加熱加圧成形した後、そのまま室
温まで冷却して厚さ1紬の積層板を得た。(Comparative Example 1) After hot-press molding in the same manner as in Example 1, the product was cooled to room temperature to obtain a laminate having a thickness of 1 pongee.
(比較IpH2ン
比較例1で得た積層板tオープンに入れ%160℃で2
時間加熱後室温に冷却して、厚さ1asの積層板を得た
。(Comparative IpH2) The laminate obtained in Comparative Example 1 was placed in an open container at 160°C.
After heating for a period of time, the mixture was cooled to room temperature to obtain a laminate having a thickness of 1 as.
(試験)
*mf!及び比較例で得た積層板の反り、ねじれ及び寸
法変化率の測定値及び表面状態を表IK示す。試験41
.500X250Mの試験片の全面tエツチングし、1
40℃で60分間加熱した後、反り、ねじれ及び加熱前
後での寸法変化を側足した0
表1
〔発明の効果〕
表1″T:BAらかなよ5に1本発明の実施例は、反り
量、ねじれ量及び寸法変化率の何れ吃従来法の比較例に
比べて少ない0反1表面の変色及び異物付着、傷、打痕
も本発明の方法によると少ないこと七確誌した〇
特に、従来から行なわれる所絹アニーリング法は、比較
912に示すように最悪の成績である。(Test) *mf! Table IK shows the measured values of warpage, twist, and dimensional change rate, and surface condition of the laminates obtained in Comparative Examples. Exam 41
.. T-etch the entire surface of a 500 x 250 M test piece,
After heating at 40°C for 60 minutes, warping, twisting, and dimensional changes before and after heating were measured. The amount of warping, amount of twisting, and rate of dimensional change are all smaller compared to the comparative example of the conventional method. It has been confirmed that the method of the present invention also has less discoloration, foreign matter adhesion, scratches, and dents on the 0-1 surface. As shown in comparison 912, the conventional annealing method has the worst performance.
Claims (1)
レグを複数枚重ね、その外面に金属箔を重ね合わせた構
成体と鏡板とを交互に重ねて加熱加圧硬化成形する積層
板の製造において、硬化成形後引続き圧を0〜20kg
/cm^3下げ、該硬化物のガラス転位温度より高い温
度で一定時間保持した後冷却することを特徴とする積層
板の製造方法。1. In the production of laminates, in which a plurality of prepregs made by impregnating and drying a thermosetting resin into a fiber base material are stacked, and a structure in which metal foil is superimposed on the outer surface and a mirror plate are alternately stacked and cured under heat and pressure. , After curing and molding, the pressure is continued from 0 to 20 kg.
/cm^3, the cured product is maintained at a temperature higher than the glass transition temperature for a certain period of time, and then cooled.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2164815A JPH0453714A (en) | 1990-06-22 | 1990-06-22 | Manufacture of laminated sheet |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2164815A JPH0453714A (en) | 1990-06-22 | 1990-06-22 | Manufacture of laminated sheet |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0453714A true JPH0453714A (en) | 1992-02-21 |
Family
ID=15800449
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2164815A Pending JPH0453714A (en) | 1990-06-22 | 1990-06-22 | Manufacture of laminated sheet |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0453714A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0387274U (en) * | 1989-12-20 | 1991-09-04 | ||
JP2010040592A (en) * | 2008-07-31 | 2010-02-18 | Kyocer Slc Technologies Corp | Manufacturing method of wiring board |
-
1990
- 1990-06-22 JP JP2164815A patent/JPH0453714A/en active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0387274U (en) * | 1989-12-20 | 1991-09-04 | ||
JPH0446934Y2 (en) * | 1989-12-20 | 1992-11-05 | ||
JP2010040592A (en) * | 2008-07-31 | 2010-02-18 | Kyocer Slc Technologies Corp | Manufacturing method of wiring board |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1824660B1 (en) | Method for deforming a thermosetting plate | |
JPH0453714A (en) | Manufacture of laminated sheet | |
JPS6365509B2 (en) | ||
JP2510638B2 (en) | Laminated board manufacturing method | |
JPH0421413A (en) | Manufacture of laminated sheet | |
JP2001179762A (en) | Method for producing laminated plate and plate for molding laminated plate | |
JP2591378B2 (en) | Manufacturing method of composite laminate | |
JP4425523B2 (en) | Laminate production method | |
JP2551032B2 (en) | Laminated board manufacturing method | |
JPS59129490A (en) | Method of producing laminated board | |
JPS602333A (en) | Manufacture of laminate plate | |
JPS58220730A (en) | Manufacture of laminated board | |
JPS587348A (en) | Manufacture of metallic foil lined laminated board | |
JPH06171052A (en) | Manufacture of laminated sheet | |
JP2002264157A (en) | Method for producing laminated plate | |
JPH04119836A (en) | Metal foil clad laminated sheet and preparation thereof | |
JPS62149427A (en) | Manufacture of copper clad laminated sheet | |
JP2963166B2 (en) | Method of manufacturing single-sided copper-clad laminate | |
JPH04201311A (en) | Manufacture of laminated sheet | |
JPS61188133A (en) | Manufacture of laminated sheet | |
JPH10166381A (en) | Manufacture of laminated plate | |
JPH0397551A (en) | Production of laminated sheet | |
JPH0367648A (en) | Manufacture of phenol resin copper clad laminated sheet | |
JPS61206647A (en) | Manufacture of laminated board | |
JPS634935A (en) | Preparation of multilayer circuit board |