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JP4070290B2 - Panel manufacturing method filled with foamed resin and panel manufacturing apparatus - Google Patents

Panel manufacturing method filled with foamed resin and panel manufacturing apparatus Download PDF

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Publication number
JP4070290B2
JP4070290B2 JP05652298A JP5652298A JP4070290B2 JP 4070290 B2 JP4070290 B2 JP 4070290B2 JP 05652298 A JP05652298 A JP 05652298A JP 5652298 A JP5652298 A JP 5652298A JP 4070290 B2 JP4070290 B2 JP 4070290B2
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foamed resin
temperature
core material
heating
surface material
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JPH11254563A (en
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宏 堀籠
克彦 梅田
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Jamco Corp
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Jamco Corp
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Description

【0001】
【発明の属する技術分野】
本発明は、発泡樹脂を充填した芯材(コア)による高強度ハニカムパネルの製造方法、および製造装置に関する。
【0002】
【従来の技術】
アルミニュウム合金箔、アラミッド繊維・クラフト紙などによるハニカムコア(蜂の巣状中空芯材)の両面に表面材を接着したハニカムパネルは、軽量であって剛性を有するので、様々な用途に使用されている。
使用目的にもよるが、一般的にハニカムパネルに要求される物理的特性は、下記の項目がある。
1.曲げ及び圧縮強度
2.接着強度
3.耐火性
4.耐久性
5.耐湿、耐水性
6.耐衝撃性
これらの特性の全てを1種類のハニカムパネルに持たせることは困難なので、それぞれの用途に応じて、表面材、芯材(コア)、接着剤の素材の選択、またはパネルの厚さ、寸法等を調整して、用途に応じた物理的要求を達成させている。例えば、ハニカムパネルに曲げモーメントが加わると、表裏の表面材にそれぞれ圧縮応力、引張り応力が発生すると共に、芯材には剪断応力が発生して、表裏の力が打ち消し合って均衝する。
このような状態において、表面材と芯材の接着は重要な意義を持っているため、強い接着強度が要求される。
【0003】
一方、芯材の中空部に水あるいは湿気が浸入、蓄積すると、芯材が湿気で腐食される不都合が発生する。あるいは、芯材と表面材を接着している接着剤が吸水して接着強度が低下し、ハニカムパネルの耐久性を損ねる結果となってしまった。
そこで、芯材の6角柱状、円筒状の中空部分への湿気(水分)の浸入の問題を解決する方法として、芯材の中空部に比重の低い発泡樹脂を充填して、水分の芯材および接着剤との接触を防止する方法が採られている。
この発泡樹脂を充填したハニカムパネルは、発泡樹脂の充填により耐久性が向上するとともに、ハニカムコア(芯材)内部の空気対流がなくなるため、パネルに断熱特性が付与されることとなった。
発泡樹脂の充填はパネルの重量増を招くため、航空機への利用などは敬遠されるが、これらの特殊用途を除いて発泡樹脂充填ハニカムパネルは耐久性が確保されるため、構造用パネルとしても使用されている。しかし、現状においては価格が高く、低価格化が要望されている。
一方、経済性の問題を解決するためハニカムコアに替えて、発泡樹脂そのものを芯材として用いたパネルがあるが、発泡樹脂の剪断剛性が低いため構造用には不適当で、断熱パネルとして使用されるに止まっている。
【0004】
ここで、発泡樹脂充填のハニカムパネルの従来の製法を説明する。
従来の製法例1.
充填樹脂に表面材の接着機能を兼ねさせる方法(図10参照)
表面材として未発泡の発泡樹脂粉を塗布した樹脂層6を積層する。あるいは樹脂を含浸させたガラス繊維の不織布5を用いる。……(a参照)
芯材3の表裏面に樹脂層6を有する不織布5を積層し、熱プレスで加熱/加圧する。……(b参照)
加熱により樹脂を発泡させると同時に、加圧して表面材となる不織布5と芯材3を接着する製造方法である。
このハニカムパネルは低価格ではあるが、芯材3と発泡樹脂6’の接着強度が低いため、高強度のパネルとしての使用には限界があった。
接着強度を高めるために、発泡樹脂の発泡倍率を抑えることも行われているが、この場合は、パネルの重量増を招いて軽量化の目的を達していない。
【0005】
従来の製法例2.
張り付けた表面材を剥離し、新しい表面材を張る方法(図11参照)
この製造方法は、製法例1で示した製法で芯材3に表面材5,6を接着させる工程(a,b参照)の後に、表面材5を機械的に剥離する(c参照)。このとき、芯材3の端部に充填されている発泡樹脂6’も一緒に除去する。次に、新たな表面材7を強度の高い接着剤8により接着する方法である。
このハニカムパネルは発泡樹脂6’と無関係に接着剤8が選定できるので、構造用に適する高強度パネルが製造できる。しかし、芯材3の端部に付着する発泡樹脂6’を完全に除去することが困難であって、新しい表面材7と芯材3の接着時に接着強度を確保するフィレット(接着剤が芯材に沿って盛り上がる部分)の形成が不確実であって、所望する接着強度が得られないという問題、および接着工程が2回となり、経済的でないことが欠点であった。
【0006】
従来の製法例3.
片面づつ表面材を接着する方法(図12参照)
先ず、芯材3の片側に表面材5を接着する(a参照)。芯材3の中空部に接着工程で発泡する粉末の発泡樹脂6’を入れる(b参照)。その後、もう片方の表面材5を接着する(c参照)方法である。
この方法によるハニカムパネルは、強度、断熱性は確保できるが、それぞれの表面材の接着強度が異なり完成したパネルに反りがで易いという問題、および接着工程が2回となり、経済的でないことが欠点であった。
以上の説明の通り、発泡樹脂を充填したハニカムパネルの製法は種々あるが、強度、重量、コストの全てを満足する製法はなかった。
【0007】
【発明が解決しようとする課題】
本発明が解決すべき課題は、発泡樹脂を充填した高強度のハニカムパネルを経済的に提供することである。
【0008】
【課題を解決するための手段】
本発明のハニカムパネルの製造方法は、表面材と芯材を接着する接着剤と、熱反応温度が異なる発泡樹脂の2層を発泡樹脂層、接着層、表面材の順に積層してプレスで加圧後、段階的に加熱温度を上昇させることによって、先ず表面材と芯材の接着剤層を溶融/硬化開始させたのち、発泡樹脂を発泡させて空間に充填させる構成を有している。
また、接着層と発泡樹脂層をフィルム状に成形し、積層工程において芯材と表面材との間にフィルム体の接着層を表面材に対向させて積層する構成を有する。
また、前記表面材は所定の温度で反応する接着剤を塗布、あるいは含浸させて形成されると共に、接着剤の熱反応温度より発泡温度が高い発泡樹脂を表面材に積層した構成を有している。
この方法は、表面材と芯材の接着において、フィレットの形成が確実にできる。
【0009】
本発明のハニカムパネルの製造装置は、芯材の上下面に発泡樹脂層と接着層とを有する表面材を該発泡樹脂層を芯材に対向させて積層する積層手段と、表面材を積層した芯材を挾持して加熱、加圧する加熱加圧手段と、加熱加圧手段の加熱温度を制御する加熱温度制御手段とを備え、加熱温度の制御手段は少なくとも接着層が反応する反応温度と発泡樹脂層が発泡する温度の制御をなす構成を具備する
【0010】
【発明の実施の形態】
図面を参照して、本発明に係るハニカムパネルの製造方法の実施の形態を説明する。
ハニカムパネル10は芯材30の両面に表面材50を2層フィルム40を介して接着して形成されている。
表面材50はシート状のアルミニューム合金を使用している。
芯材30はアルミニュウム合金箔材による6角筒状(ハニカム)の芯材を用いている。
芯材30には図4(a)に示すように、断面6角形の筒状を連続形成するハニカムコア、あるいは(b)に示すように、断面丸形の円筒を連続形成するロ−ルコアがある。
2層樹脂フィルム40は、ガラス繊維の担持体41を有するエポキシ樹脂接着剤層42と、発泡フェノール層44を積層してシ−ト状としている。……図3参照
【0011】
これらの素材を用いて、高強度のハニカムパネル10を形成する工程を説明する。……図1参照
第1工程.(a)
芯材30の両面に、2層樹脂フィルム40のエポキシ樹脂接着剤層42を表面材50に対向させて重ね合わせる。
第2工程.(b)
芯材30と2層樹脂フィルム40と表面材50とを積層した積層材をプレス装置にかけ、常温状態のプレスで圧着する。芯材30に圧迫された発泡フェノール層44は破壊されて、芯材30はエポキシ接着剤層42に食い込み圧接される。この状態で、プレスの温度を125℃に上昇させる。125℃程度の温度でエポキシ樹脂接着剤層42は溶融する。そして、所定の時間後硬化を始める。
【0012】
第3工程.(c)
プレスの温度を更に180℃まで昇温させて加熱する。
この温度で発泡フェノール層44の発泡樹脂が発泡する。発泡した樹脂は芯材30の空間を充填し、発泡層440を形成する。
このまま20分間180℃の温度を保持する。
この間にエポキシ樹脂接着剤層42の硬化が完了する。
150℃まで冷却させてパネル10をプレス装置から外し、垂直に立てかけて常温まで冷却して完成させる。
【0013】
この例では表面材と芯材の接着剤としてエポキシ樹脂を用いたが、フェノール樹脂、ナイロン樹脂などの接着強度の高い樹脂を用いても良い。
発泡樹脂としてはフェノール樹脂の例を示したが、ウレタン樹脂、スチロール樹脂を用いても良い。
表面材としては、アルミニューム合金シートの他に、炭素繊維、ガラス繊維の織布が用いられる。芯材にはアラミツド繊維紙、不燃紙(無機ペーパー)、クラフト紙などの材料を6角筒状、あるいは円筒状に成形したものを用いる。
【0014】
上記製造方法で形成したハニカムパネルの強度試験を実行した。
試験の結果、芯材として高強度で薄肉のアルミニューム合金ハニカムコアを用いたパネルが、特に高強度を示した。これは薄肉のアルミニューム合金の芯材(コア)端部が鋭いため、第2工程において、接着剤層への喰い込み度合いが強く、図5に示すような、芯材30の端部に接着剤42が盛り上がるフィレット420が確実に形成される。このため、接着強度が高まり、コア端部への発泡樹脂層440の形成を排除し、表面材50と芯材30とが直接接着されるためと考えられる。
芯材と接着層との接着強度は、芯材の切断(スライス加工)に用いる鋸の刃のあさりを強くして、芯材端面の凹凸を激しくすることにより接着層への食い込みを強くする手段を用いることもできる。この場合も、芯材と表面材との接着部分の発泡樹脂の影響を排除して接着強度を高めることができる。
その他、図6に示すように、発泡樹脂材層44に予め鋭い凹凸あるいは切り込み45を配設する。そして、この切り込み45に芯材の端部を食い込ませる方法も有効である。
【0015】
この形態の製造方法を実施するプレス装置を説明する。
〈実施例1〉
一台のプレスを使って加熱温度の制御によりパネルを一枚づつ製造する装置。
この場合のプレス装置の温度制御を図2に示す。
第1工程においては常温で各部材の積層を行う。第2工程の開始時間t1には温度を125℃に昇温させる。接着樹脂が溶融する所定の時間が経過した後、時間t2から温度を180℃に昇温させる。第3工程において発泡樹脂が発泡して芯材中に充填が終了する時間t3まで、約20分間、180℃を保持する。そして、加熱を終了させて自然冷却とする。
【0016】
〈実施例2〉
このプレス装置は、設定温度を常温とする常温プレス機71、設定温度を125℃とする中温プレス機73、設定温度を180℃とする高温プレス機75の3台のプレス機を別体に配設する。そして、一枚のパネルを常温プレス機71、中温プレス機73、高温プレス機75の順に順次通過させて、常温プレス機71で材料を圧接した後、中温プレス機73で加熱/加圧して表面材と芯材の接着を進行させ、さらに高温プレス機73で加熱/加圧して発泡樹脂を芯材中に発泡充填させる。
このプレス装置は発泡樹脂を充填させたハニカムパネルを、一枚づつ製造する。
【0017】
〈実施例3〉
このプレス装置80は設定温度を常温とする常温プレス台81、設定温度を125℃とする中温プレス台83、設定温度を180℃とする高温プレス台85を直列に配設している。
芯材30の上下面にロール状に巻いた2層樹脂フィルム40を積層した表面材50を載置し、芯材30の進行に合わせて、2層樹脂フィルム40を積層した表面材50を巻き解しながら芯材30に重合して行く。表面材50を積層した芯材30はプレス台81,83,85の間隔寸法に合わせて間歇的に移動させる。先ず、積層体は常温プレス台81にプレスされて芯材30端部が接着剤層に食い込む。この状態でプレスを解除して、表面材50を積層した芯材30を所定の距離移動させる。中温プレス台83位置において、接着剤層が溶け、芯材30と表面材50が接着する。中温プレス台83を解除して、表面材50を接着した芯材30を所定の距離移動させる。高温プレス台85位置において、発泡樹脂層が発泡して芯材30の中空部分を充填する。高温プレス台85を解除して発泡充填を完了したパネルはさらに所定の距離移動しながら、徐々に室温に冷却してゆく。
【0018】
このプレス装置80は工程を間欠的に連続自動化させてパネルを形成している。3台のプレス台81,83,85は、完全に同期させており、加圧・除圧を間欠的に繰り返し、除圧時にパネルを適当な長さだけ移動させて、連続してパネルを製造する。プレス台の加圧・除圧時間、およびパネルの送り速度は樹脂の材料、あるいは加熱口ーラーの温度設定などの条件から決定される。
また、この実施例は表面材をアルミニューム合金とし、予め2層樹脂フィルムを片面に重合した表面材をロール状に巻い状態とした例を示しているが、表面材にガラス繊維あるいは炭素繊維を用いる場合には、繊維地(表面材)に予め半硬化させた接着樹脂を含浸させておき(この状態の布地は通称プリプレグと呼ばれている)、プリプレグの表面に発泡充填する発泡樹脂をコーティングして表面材としても良い。
【0019】
〈実施例4〉
このプレス装置90は設定温度を常温とする一対の常温プレスロールを2台、プレスロール91A,91Bを併設する。その下流側に設定温度を125℃とする2台の中温プレスロール93A,93Bを併設、さらに下流側に設定温度を180℃とする2台の高温プレスロール95A,95Bを併設している。
芯材30の上下面にロール状に巻いた2層樹脂フィルム40を積層した表面材50を載置し、所定の速度で芯材30に、2層樹脂フィルム40を積層した表面材50を巻き解しながら重合して行く。表面材50を積層した芯材30は常温プレスロール91A,91Bにプレスされて芯材30端部が接着剤層に食い込む。この状態で進行する表面材50に積層された芯材30は中温プレスロール93A,93Bにより、接着剤層が溶解し、芯材30と表面材50が接着する。中温プレスロール93A,93Bを通過した表面材50を接着した芯材30は、高温プレスロール95A,95B位置において、発泡樹脂層が発泡して芯材30の中空部分を充填する。発泡充填を完了したパネルはさらに所定の距離移動しながら、徐々に室温に冷却してゆく。
【0020】
このプレス装置90は連続自動的に発泡樹脂を充填したパネルを製造する。すなわち、上下2本の加熱/加圧ロールを3組併設し、所定の速度で連続的に移動させることにより、連続したパネルを形成することが出来る。芯材30の送り速度は樹脂の材料と加熱口ールの温度設定などの条件から決定される。
この場合も、プリプレグの表面に発泡充填する発泡樹脂をコーティングした表面材を用いることができる。
【0021】
【発明の効果】
本発明によって、発泡樹脂を充填した高い強度を有するハニカムパネルの形成が容易に、かつ経済的に提供することができる。
【図面の簡単な説明】
【図1】本発明による製造方法の工程説明図。
【図2】加熱温度の変化を示すグラフ。
【図3】接着/発泡樹脂2層フィルムの拡大図。
【図4】芯材(通称ハニカムコア)の上面図。
【図5】フイレットの形成説明図。
【図6】2層フィルムの他の例を示す拡大図。
【図7】プレス装置の第1の実施例を示す説明図。
【図8】プレス装置の第2の実施例を示す説明図。
【図9】プレス装置の第3の実施例を示す説明図。
【図10】従来のプレス方法の工程説明図。
【図11】従来のプレス方法の工程説明図。
【図12】従来のプレス方法の工程説明図。
【符号の説明】
10 ハニカムパネル
30 芯材
40 2層フィルム
41 ガラス繊維の担持体
42 エポキシ樹脂接着剤層
44 発泡フェノール層
50 表面材
71 常温プレス機
73 中温プレス機
75 高温プレス機
80,90 プレス装置
81 常温プレス台
83 中温プレス台
85 高温プレス台
91A,91B プレスロール
93A,93B 中温プレスロール
95A,95B 高温プレスロール
420 フィレット
440 発泡層
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a manufacturing method and a manufacturing apparatus for a high-strength honeycomb panel using a core material (core) filled with foamed resin.
[0002]
[Prior art]
A honeycomb panel in which a surface material is bonded to both sides of a honeycomb core (honeycomb-shaped hollow core material) made of aluminum alloy foil, aramid fiber, kraft paper, or the like is lightweight and rigid, and thus is used in various applications.
Although depending on the purpose of use, the physical properties generally required for honeycomb panels include the following items.
1. 1. Bending and compressive strength 2. Adhesive strength Fire resistance4. Durability 5. 5. Moisture and water resistance Impact resistance Since it is difficult to have all of these characteristics in one type of honeycomb panel, depending on the application, the choice of surface material, core material (core), adhesive material, or panel thickness The physical requirements according to the application are achieved by adjusting the dimensions and the like. For example, when a bending moment is applied to the honeycomb panel, a compressive stress and a tensile stress are generated on the front and back surface materials, respectively, and a shear stress is generated on the core material, so that the front and back forces cancel each other and balance each other.
In such a state, since the adhesion between the surface material and the core material has an important significance, a strong adhesive strength is required.
[0003]
On the other hand, when water or moisture enters and accumulates in the hollow portion of the core material, there arises a problem that the core material is corroded by moisture. Or the adhesive which adhere | attached the core material and the surface material absorbed water, the adhesive strength fell, and it resulted in impairing the durability of a honeycomb panel.
Therefore, as a method of solving the problem of moisture (moisture) permeation into the hexagonal columnar or cylindrical hollow portion of the core material, the core material of water is filled with a foam resin having a low specific gravity in the hollow portion of the core material. And a method of preventing contact with the adhesive.
The honeycomb panel filled with the foamed resin has improved durability due to the filling of the foamed resin, and air convection inside the honeycomb core (core material) is eliminated, so that a heat insulating property is imparted to the panel.
Filling with foamed resin causes an increase in the weight of the panel, so use in aircraft is avoided.However, except for these special applications, the foamed resin-filled honeycomb panel ensures durability, so it can be used as a structural panel. in use. However, at present, the price is high, and there is a demand for lower prices.
On the other hand, there is a panel that uses foamed resin itself as a core material instead of a honeycomb core to solve economic problems, but it is not suitable for structural use due to the low shear rigidity of foamed resin, and used as a heat insulation panel It has been stopped.
[0004]
Here, a conventional method for manufacturing a honeycomb panel filled with foamed resin will be described.
Example of conventional manufacturing method
Method to make the filling resin also have the adhesive function of the surface material (see Fig. 10)
A resin layer 6 coated with unfoamed foamed resin powder is laminated as a surface material. Alternatively, a glass fiber nonwoven fabric 5 impregnated with resin is used. (Refer to a)
A nonwoven fabric 5 having a resin layer 6 is laminated on the front and back surfaces of the core material 3 and heated / pressurized by hot pressing. (Refer to b)
In this manufacturing method, the resin is foamed by heating, and at the same time, the nonwoven fabric 5 and the core material 3 are bonded by pressing to form a surface material.
Although this honeycomb panel is low in price, its use as a high-strength panel is limited because the adhesive strength between the core material 3 and the foamed resin 6 'is low.
In order to increase the adhesive strength, the expansion ratio of the foamed resin is also suppressed, but in this case, the weight of the panel is increased and the purpose of reducing the weight is not achieved.
[0005]
Conventional manufacturing method example 2
A method of peeling the attached surface material and applying a new surface material (see Fig. 11)
In this manufacturing method, the surface material 5 is mechanically peeled off (see c) after the step (see a and b) of bonding the surface materials 5 and 6 to the core material 3 by the manufacturing method shown in the manufacturing method example 1. At this time, the foamed resin 6 ′ filled in the end portion of the core material 3 is also removed together. Next, a new surface material 7 is bonded by a high strength adhesive 8.
Since this honeycomb panel can select the adhesive 8 irrespective of the foamed resin 6 ', a high-strength panel suitable for the structure can be manufactured. However, it is difficult to completely remove the foamed resin 6 ′ adhering to the end portion of the core material 3, and a fillet (adhesive is used as the core material) that secures adhesive strength when the new surface material 7 and the core material 3 are bonded. The problem is that the formation of the portion that swells along the line is uncertain, the desired adhesive strength cannot be obtained, and the bonding process is twice, which is not economical.
[0006]
2. Conventional manufacturing method example 3
Method of bonding surface materials one side at a time (see Fig. 12)
First, the surface material 5 is bonded to one side of the core material 3 (see a). A powdered foamed resin 6 ′ that foams in the bonding step is placed in the hollow portion of the core material 3 (see b). Thereafter, the other surface material 5 is bonded (see c).
Honeycomb panels by this method can ensure strength and heat insulation, but the problem is that the surface panels have different adhesive strengths, and the finished panel tends to warp, and the bonding process is twice, which is not economical. Met.
As described above, there are various methods for manufacturing a honeycomb panel filled with a foamed resin, but there is no method that satisfies all of the strength, weight, and cost.
[0007]
[Problems to be solved by the invention]
The problem to be solved by the present invention is to economically provide a high-strength honeycomb panel filled with foamed resin.
[0008]
[Means for Solving the Problems]
In the method for manufacturing a honeycomb panel of the present invention, two layers of an adhesive for adhering a surface material and a core material and a foamed resin having different thermal reaction temperatures are laminated in the order of the foamed resin layer, the adhesive layer, and the surface material, and then added by a press. After pressurization, the heating temperature is raised stepwise to first start melting / curing the adhesive layer of the surface material and the core material, and then foam the foamed resin to fill the space.
Further, by forming the adhesive layer and the foamed resin layer in a film shape, having you laminate constituting the adhesive layer of the film body to face the surface material between the core material and surface material in the lamination process.
The surface material is formed by applying or impregnating an adhesive that reacts at a predetermined temperature, and has a structure in which a foamed resin having a foaming temperature higher than the thermal reaction temperature of the adhesive is laminated on the surface material. Yes.
The method Oite the adhesion of the surface material and core material, the formation of the fillet can be reliably.
[0009]
The honeycomb panel manufacturing apparatus of the present invention includes a stacking means for stacking a surface material having a foamed resin layer and an adhesive layer on the upper and lower surfaces of the core material with the foamed resin layer facing the core material, and the surface material. A heating / pressurizing unit that holds and heats and presses the core material, and a heating temperature control unit that controls the heating temperature of the heating / pressurizing unit. The heating temperature control unit includes at least a reaction temperature and foaming at which the adhesive layer reacts. The structure which controls the temperature which a resin layer foams is comprised .
[0010]
DETAILED DESCRIPTION OF THE INVENTION
Embodiments of a method for manufacturing a honeycomb panel according to the present invention will be described with reference to the drawings.
The honeycomb panel 10 is formed by adhering a surface material 50 to both surfaces of a core material 30 via a two-layer film 40.
The surface material 50 uses a sheet-like aluminum alloy.
The core material 30 is a hexagonal cylindrical (honeycomb) core material made of an aluminum alloy foil material.
As shown in FIG. 4 (a), the core 30 has a honeycomb core that continuously forms a hexagonal cross section, or a roll core that continuously forms a round cross section cylinder as shown in (b). is there.
The two-layer resin film 40 is formed into a sheet by laminating an epoxy resin adhesive layer 42 having a glass fiber carrier 41 and a foamed phenol layer 44. ...... See Figure 3 [0011]
A process for forming the high-strength honeycomb panel 10 using these materials will be described. ...... Refer to FIG. 1 First step. (A)
The epoxy resin adhesive layer 42 of the two-layer resin film 40 is superimposed on both surfaces of the core material 30 so as to face the surface material 50.
Second step. (B)
The laminated material obtained by laminating the core material 30, the two-layer resin film 40 and the surface material 50 is applied to a press device and is pressure-bonded by a press at a normal temperature. The foamed phenol layer 44 pressed against the core material 30 is destroyed, and the core material 30 bites into the epoxy adhesive layer 42 and is pressed. In this state, the temperature of the press is raised to 125 ° C. The epoxy resin adhesive layer 42 melts at a temperature of about 125 ° C. Then, curing is started after a predetermined time.
[0012]
Third step. (C)
The temperature of the press is further raised to 180 ° C. and heated.
At this temperature, the foamed resin of the foamed phenol layer 44 is foamed. The foamed resin fills the space of the core material 30 and forms the foam layer 440.
The temperature of 180 ° C. is maintained for 20 minutes.
During this time, curing of the epoxy resin adhesive layer 42 is completed.
The panel 10 is removed from the press device by cooling to 150 ° C., and is vertically stood to cool to room temperature to complete.
[0013]
In this example, an epoxy resin is used as an adhesive between the surface material and the core material, but a resin having high adhesive strength such as a phenol resin or a nylon resin may be used.
Although the example of the phenol resin was shown as foamed resin, you may use a urethane resin and a styrene resin.
As the surface material, in addition to the aluminum alloy sheet, a woven fabric of carbon fiber or glass fiber is used. As the core material, a material such as aramid fiber paper, non-combustible paper (inorganic paper), craft paper or the like formed into a hexagonal cylindrical shape or a cylindrical shape is used.
[0014]
A strength test of the honeycomb panel formed by the above manufacturing method was performed.
As a result of the test, a panel using a high-strength, thin-walled aluminum alloy honeycomb core as the core material showed particularly high strength. This is because the end of the core material (core) of the thin aluminum alloy is sharp, and the degree of biting into the adhesive layer is strong in the second step, and it adheres to the end of the core material 30 as shown in FIG. The fillet 420 in which the agent 42 swells is reliably formed. For this reason, it is considered that the adhesive strength increases, the formation of the foamed resin layer 440 at the end of the core is eliminated, and the surface material 50 and the core material 30 are directly bonded.
The adhesive strength between the core material and the adhesive layer is a means to increase the biting into the adhesive layer by increasing the roughness of the saw blade used for cutting (slicing) the core material and increasing the unevenness of the end surface of the core material Can also be used. Also in this case, the adhesive strength can be increased by eliminating the influence of the foamed resin at the bonding portion between the core material and the surface material.
In addition, as shown in FIG. 6, sharp irregularities or cuts 45 are provided in advance in the foamed resin material layer 44. A method of biting the end of the core material into the notch 45 is also effective.
[0015]
The press apparatus which implements the manufacturing method of this form is demonstrated.
<Example 1>
A device that manufactures panels one by one by controlling the heating temperature using a single press.
FIG. 2 shows the temperature control of the press device in this case.
In the first step, each member is laminated at room temperature. The temperature is raised to 125 ° C. at the start time t 1 of the second step. After a predetermined time for the adhesive resin to melt, the temperature is raised to 180 ° C. from time t 2 . In the third step, the temperature is maintained at 180 ° C. for about 20 minutes until time t 3 when the foamed resin is foamed and filling into the core material is completed. And heating is complete | finished and it is set as natural cooling.
[0016]
<Example 2>
This press machine has three press machines: a normal temperature press machine 71 that sets the set temperature to room temperature, an intermediate temperature press machine 73 that sets the set temperature to 125 ° C, and a high temperature press machine 75 that sets the set temperature to 180 ° C. Set up. Then, a single panel is sequentially passed through the room temperature press machine 71, the medium temperature press machine 73, and the high temperature press machine 75 in order, and the material is pressed by the room temperature press machine 71, and then heated / pressurized by the medium temperature press machine 73. Adhesion between the core material and the core material is allowed to proceed, and further, heating / pressurization is performed by a high-temperature press machine 73 to foam and fill the core material with foamed resin.
This press machine produces honeycomb panels filled with foamed resin one by one.
[0017]
<Example 3>
The press device 80 includes a room temperature press table 81 having a set temperature of room temperature, a medium temperature press table 83 having a set temperature of 125 ° C., and a high temperature press table 85 having a set temperature of 180 ° C. arranged in series.
A surface material 50 in which a two-layer resin film 40 wound in a roll is laminated is placed on the upper and lower surfaces of the core material 30, and the surface material 50 in which the two-layer resin film 40 is laminated is wound according to the progress of the core material 30. It is polymerized to the core material 30 while solving. The core material 30 on which the surface material 50 is laminated is moved intermittently according to the distance between the press bases 81, 83, 85. First, the laminated body is pressed by the room temperature press stand 81 and the end portion of the core material 30 bites into the adhesive layer. In this state, the press is released, and the core material 30 on which the surface material 50 is laminated is moved by a predetermined distance. At the intermediate temperature press stand 83 position, the adhesive layer melts, and the core material 30 and the surface material 50 adhere. The intermediate temperature press stand 83 is released, and the core material 30 to which the surface material 50 is bonded is moved by a predetermined distance. At the position of the high-temperature press stand 85, the foamed resin layer foams and fills the hollow portion of the core material 30. The panel after releasing the high-temperature press stand 85 and completing foam filling is gradually cooled to room temperature while moving a predetermined distance.
[0018]
The press device 80 forms a panel by intermittently and continuously automating the process. The three press stands 81, 83, and 85 are completely synchronized, and pressurization and depressurization are repeated intermittently, and the panel is moved by an appropriate length during depressurization to continuously produce panels. To do. The press table pressurization / decompression time and the panel feed rate are determined from conditions such as the resin material or the temperature setting of the heating porter.
In addition, this example shows an example in which the surface material is an aluminum alloy, and a surface material obtained by polymerizing a two-layer resin film on one side in advance is wound into a roll shape, but the surface material is made of glass fiber or carbon fiber. When used, fiber fabric (surface material) is impregnated with a semi-cured adhesive resin in advance (the fabric in this state is commonly called a prepreg), and the surface of the prepreg is coated with a foam resin that fills with foam. And it is good also as a surface material.
[0019]
<Example 4>
This press device 90 is provided with two pairs of room temperature press rolls having a set temperature of room temperature, and press rolls 91A and 91B. Two medium temperature press rolls 93A and 93B having a set temperature of 125 ° C. are provided on the downstream side, and two high temperature press rolls 95A and 95B having a set temperature of 180 ° C. are provided on the downstream side.
The surface material 50 in which the two-layer resin film 40 wound in a roll shape is stacked on the upper and lower surfaces of the core material 30 is placed, and the surface material 50 in which the two-layer resin film 40 is stacked on the core material 30 is wound at a predetermined speed. Polymerize while solving. The core material 30 on which the surface material 50 is laminated is pressed by the room temperature press rolls 91A and 91B, and the end of the core material 30 bites into the adhesive layer. The core material 30 laminated on the surface material 50 proceeding in this state is melted by the intermediate temperature press rolls 93A and 93B, and the core material 30 and the surface material 50 are bonded. In the core material 30 to which the surface material 50 that has passed the intermediate temperature press rolls 93A and 93B is bonded, the foamed resin layer foams and fills the hollow portion of the core material 30 at the high temperature press rolls 95A and 95B positions. The panel which has completed foam filling is gradually cooled to room temperature while moving a predetermined distance.
[0020]
This press device 90 continuously and automatically manufactures a panel filled with foamed resin. That is, a continuous panel can be formed by providing three sets of two upper / lower heating / pressurizing rolls and continuously moving them at a predetermined speed. The feed rate of the core material 30 is determined from conditions such as the resin material and the temperature setting of the heating nozzle.
Also in this case, a surface material obtained by coating the surface of the prepreg with a foamed resin to be foam-filled can be used.
[0021]
【The invention's effect】
According to the present invention, it is possible to easily and economically provide a high strength honeycomb panel filled with foamed resin.
[Brief description of the drawings]
FIG. 1 is a process explanatory diagram of a production method according to the present invention.
FIG. 2 is a graph showing changes in heating temperature.
FIG. 3 is an enlarged view of an adhesive / foamed resin bilayer film.
Fig. 4 is a top view of a core material (commonly called a honeycomb core).
FIG. 5 is a diagram illustrating the formation of a fillet.
FIG. 6 is an enlarged view showing another example of a two-layer film.
FIG. 7 is an explanatory view showing a first embodiment of the press device.
FIG. 8 is an explanatory view showing a second embodiment of the press device.
FIG. 9 is an explanatory view showing a third embodiment of the press device.
FIG. 10 is a process explanatory diagram of a conventional pressing method.
FIG. 11 is a process explanatory diagram of a conventional pressing method.
FIG. 12 is a process explanatory diagram of a conventional pressing method.
[Explanation of symbols]
DESCRIPTION OF SYMBOLS 10 Honeycomb panel 30 Core material 40 Two layer film 41 Glass fiber carrier 42 Epoxy resin adhesive layer 44 Foamed phenol layer 50 Surface material 71 Room temperature press machine 73 Medium temperature press machine 75 High temperature press machine 80, 90 Press apparatus 81 Room temperature press stand 83 Medium temperature press stand 85 High temperature press stand 91A, 91B Press roll 93A, 93B Medium temperature press roll 95A, 95B High temperature press roll 420 Fillet 440 Foam layer

Claims (4)

発泡樹脂を充填した芯材の上下面に表面材を積層したパネルの製造方法において、
中空柱体を併設する芯材の上下面に、発泡樹脂層、接着層、表面材の順に積層する積層工程と、
接着層が熱反応する温度で加熱加圧する接着工程と、
発泡樹脂層が発泡する温度で加熱加圧する充填工程とを備え、
接着層の熱反応温度は発泡樹脂の発泡温度より低く設定すると共に、各工程は段階的に設定した加熱温度により接着、発泡を実行させるよう構成してなる発泡樹脂を充填したパネルの製造方法。
In the manufacturing method of the panel in which the surface material is laminated on the upper and lower surfaces of the core material filled with the foam resin,
A lamination step of laminating a foamed resin layer, an adhesive layer, and a surface material in this order on the upper and lower surfaces of the core material with the hollow column;
An adhesion process in which the adhesive layer is heated and pressurized at a temperature at which the thermal reaction occurs;
And a filling step of heating and pressurizing at a temperature at which the foamed resin layer foams,
A method for producing a panel filled with a foamed resin, wherein the thermal reaction temperature of the adhesive layer is set lower than the foaming temperature of the foamed resin, and each step is configured to perform adhesion and foaming by a stepwise set heating temperature.
芯材の上下面に配設する、発泡樹脂層、接着層は、接着層発泡樹脂層を積層したフィルム体よりなり、積層工程において芯材と表面材との間にフィルム体の接着層を表面材に対向させて積層するよう構成してなる請求項1記載の発泡樹脂を充填したパネルの製造方法。The foamed resin layer and adhesive layer disposed on the upper and lower surfaces of the core material are composed of a film body in which the adhesive layer and the foamed resin layer are laminated, and the film body adhesive layer is provided between the core material and the surface material in the lamination process . The manufacturing method of the panel filled with the foamed resin of Claim 1 comprised so that it might oppose and laminate | stack on a surface material . 発泡樹脂を充填した芯材の上下面に表面材を積層したパネルの製造方法において、
前記表面材は所定の温度で反応する接着剤を塗布、あるいは含浸させて形成されると共に、接着剤の熱反応温度より発泡温度が高い発泡樹脂を表面材に積層して構成され
中空柱体を併設する芯材の上下面に、表面材を積層する積層工程と、
前記接着剤が溶融する温度で加熱加圧する接着工程と、
発泡樹脂層が発泡する温度で加熱加圧する充填工程とを備え、
前記接着工程、充填工程は段階的に設定した異なる加熱温度により接着、発泡を実行させるよう構成してなる発泡樹脂を充填したパネルの製造方法。
In the manufacturing method of the panel in which the surface material is laminated on the upper and lower surfaces of the core material filled with the foam resin,
The surface material is formed by applying or impregnating an adhesive that reacts at a predetermined temperature, and is formed by laminating a foamed resin having a foaming temperature higher than the thermal reaction temperature of the adhesive on the surface material ,
The upper and lower surfaces of the core material which houses a hollow pillar, and a laminating step of laminating the surface member,
An adhesion step of heating and pressing at a temperature at which the adhesive melts;
And a filling step of heating and pressurizing at a temperature at which the foamed resin layer foams,
The method for manufacturing a panel filled with a foamed resin, wherein the bonding step and the filling step are configured to perform bonding and foaming at different heating temperatures set in stages.
芯材の上下面に発泡樹脂層と接着層とを有する表面材を該発泡樹脂層を芯材に対向させて積層する積層手段と、
表面材を積層した芯材を挾持して加熱、加圧する加熱加圧手段と、
加熱加圧手段の加熱温度を制御する加熱温度制御手段とを備え、
加熱温度の制御手段は少なくとも接着層が反応する反応温度と発泡樹脂層が発泡する温度の制御をなすよう構成されてなるパネルの製造装置。
Laminating means for laminating a surface material having a foamed resin layer and an adhesive layer on the upper and lower surfaces of the core material with the foamed resin layer facing the core material ;
Heating and pressurizing means for holding and heating the core material laminated with the surface material;
A heating temperature control means for controlling the heating temperature of the heating and pressurizing means,
The apparatus for manufacturing a panel, wherein the heating temperature control means is configured to control at least the reaction temperature at which the adhesive layer reacts and the temperature at which the foamed resin layer foams .
JP05652298A 1998-03-09 1998-03-09 Panel manufacturing method filled with foamed resin and panel manufacturing apparatus Expired - Fee Related JP4070290B2 (en)

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