JPH0232840A - Composite reinforced plastic prepared by laminating air-tight reinforcing material - Google Patents
Composite reinforced plastic prepared by laminating air-tight reinforcing materialInfo
- Publication number
- JPH0232840A JPH0232840A JP18156888A JP18156888A JPH0232840A JP H0232840 A JPH0232840 A JP H0232840A JP 18156888 A JP18156888 A JP 18156888A JP 18156888 A JP18156888 A JP 18156888A JP H0232840 A JPH0232840 A JP H0232840A
- Authority
- JP
- Japan
- Prior art keywords
- reinforcing material
- sheet
- plastic
- reinforcing
- hole diameter
- 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
- 239000012779 reinforcing material Substances 0.000 title claims abstract description 21
- 239000002131 composite material Substances 0.000 title claims abstract description 8
- 239000002990 reinforced plastic Substances 0.000 title claims abstract description 8
- 238000010030 laminating Methods 0.000 title 1
- 239000004033 plastic Substances 0.000 claims abstract description 26
- 229920003023 plastic Polymers 0.000 claims abstract description 26
- 229910052751 metal Inorganic materials 0.000 claims abstract description 15
- 239000002184 metal Substances 0.000 claims abstract description 15
- 229920005989 resin Polymers 0.000 claims abstract description 12
- 239000011347 resin Substances 0.000 claims abstract description 12
- 239000011888 foil Substances 0.000 claims abstract description 8
- 230000003014 reinforcing effect Effects 0.000 claims description 18
- 229920001187 thermosetting polymer Polymers 0.000 claims description 5
- 229920005992 thermoplastic resin Polymers 0.000 claims description 3
- 238000005553 drilling Methods 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 claims 1
- 229910052782 aluminium Inorganic materials 0.000 abstract description 10
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 10
- 238000000034 method Methods 0.000 abstract description 8
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 abstract description 6
- 238000004080 punching Methods 0.000 abstract description 6
- 239000002985 plastic film Substances 0.000 abstract description 4
- 229910052742 iron Inorganic materials 0.000 abstract description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 abstract description 2
- 229910052802 copper Inorganic materials 0.000 abstract description 2
- 239000010949 copper Substances 0.000 abstract description 2
- 238000010894 electron beam technology Methods 0.000 abstract description 2
- 229920006255 plastic film Polymers 0.000 abstract description 2
- 229910001220 stainless steel Inorganic materials 0.000 abstract description 2
- 239000010935 stainless steel Substances 0.000 abstract description 2
- 230000002787 reinforcement Effects 0.000 abstract 2
- 239000000463 material Substances 0.000 description 8
- 239000003822 epoxy resin Substances 0.000 description 7
- 229920000647 polyepoxide Polymers 0.000 description 7
- 229920002292 Nylon 6 Polymers 0.000 description 5
- 239000000835 fiber Substances 0.000 description 5
- 239000010410 layer Substances 0.000 description 5
- 239000004809 Teflon Substances 0.000 description 3
- 229920006362 Teflon® Polymers 0.000 description 3
- 229910010293 ceramic material Inorganic materials 0.000 description 3
- 229920001721 polyimide Polymers 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- 239000004642 Polyimide Substances 0.000 description 2
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- 230000008602 contraction Effects 0.000 description 2
- 230000032798 delamination Effects 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000035699 permeability Effects 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 239000004593 Epoxy Substances 0.000 description 1
- 229930182556 Polyacetal Natural products 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 229920000265 Polyparaphenylene Polymers 0.000 description 1
- 239000004721 Polyphenylene oxide Substances 0.000 description 1
- 239000004734 Polyphenylene sulfide Substances 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- NBVXSUQYWXRMNV-UHFFFAOYSA-N fluoromethane Chemical compound FC NBVXSUQYWXRMNV-UHFFFAOYSA-N 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 150000003949 imides Chemical class 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- OOYGSFOGFJDDHP-KMCOLRRFSA-N kanamycin A sulfate Chemical group OS(O)(=O)=O.O[C@@H]1[C@@H](O)[C@H](O)[C@@H](CN)O[C@@H]1O[C@H]1[C@H](O)[C@@H](O[C@@H]2[C@@H]([C@@H](N)[C@H](O)[C@@H](CO)O2)O)[C@H](N)C[C@@H]1N OOYGSFOGFJDDHP-KMCOLRRFSA-N 0.000 description 1
- 239000002648 laminated material Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 239000012778 molding material Substances 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 239000004417 polycarbonate Substances 0.000 description 1
- 229920000515 polycarbonate Polymers 0.000 description 1
- 238000006068 polycondensation reaction Methods 0.000 description 1
- 229920000570 polyether Polymers 0.000 description 1
- 229920000098 polyolefin Polymers 0.000 description 1
- 229920006324 polyoxymethylene Polymers 0.000 description 1
- -1 polyphenylene Polymers 0.000 description 1
- 229920000069 polyphenylene sulfide Polymers 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
Abstract
Description
【発明の詳細な説明】
イ 産業上の利用分野
本発明は車輛、航空機その他構造用材料及び電子機器用
の電磁遮蔽材料・回路基板その他の部材などに用いられ
るテープ状板状の強化プラスチックス分野に関するもの
である。DETAILED DESCRIPTION OF THE INVENTION A. Field of Industrial Application The present invention relates to the field of tape-like and plate-like reinforced plastics used for vehicles, aircraft and other structural materials, electromagnetic shielding materials for electronic devices, circuit boards, and other members. It is related to.
従って射出成型用材料には不適である。Therefore, it is unsuitable as an injection molding material.
p 従来技術
強化プラスチック材料の強化法としてガラス繊維、カー
ボン線維、セラミック材、金属繊維、金属コーテング繊
維などを補強材として各種プラスチックスな含浸して製
作されているが金属代替材料としては靭性(弾性率及び
衝撃強さ)層間剥離(層間破壊靭性)が劣るとされてお
り、繊維系での強化プラスチックスでは、高温(150
℃以上連続使用温度)での異方性収縮に問題を残してい
てコストが割高となっている。P Conventional technology Reinforced plastic materials are manufactured by impregnating various plastics with glass fiber, carbon fiber, ceramic materials, metal fibers, metal coated fibers, etc. as reinforcing materials. The delamination (interlaminar fracture toughness) is said to be poor, and fiber-based reinforced plastics have a high temperature (150
However, the cost remains high due to the problem of anisotropic shrinkage at temperatures above ℃ (continuous use).
ハ 発明が解決しようとする問題点
複合強化プラスチックス積層板の欠点である靭性・層間
剥離性・高温時異方収縮性などの特性向上を狙ったもの
で軽量・強靭な複合プラスチックスを成形することにあ
る。特に補強材として高価なカーボンファイバー・金属
繊維・セラミック材料などを安価な材料に代替すること
が要望されている@
二 問題点を解決する為の手段
本発明は綱状補強材をより合理的に追求したものである
。C. Problems to be solved by the invention The invention aims to improve properties such as toughness, delamination, and anisotropic shrinkage at high temperatures, which are disadvantages of composite reinforced plastic laminates, and molds lightweight and strong composite plastics. There is a particular thing. In particular, there is a demand for replacing expensive carbon fibers, metal fibers, ceramic materials, etc. with inexpensive materials as reinforcing materials. This is what I pursued.
通常綱状物は通気性・透過性をもたせるので開孔率が3
0%以上のものであるため綱を構成する素材のもつ引張
り強度・伸び率・曲げ弾性率などの特性が大きく変化し
特性によっては50係以上劣化するのが常識とされてい
る。よってこの綱状物の素材の特性値が加暢以下の劣化
に止まる範囲に小孔を搾孔することにより大きな補強効
果を実現したものである。即ち、補強材に、3.9m以
下の小孔を面積当りの開孔率として20係以下になる如
く搾孔することにより強化用プラスチックスが補強材の
上下を貫通して立体構造をもつこととなり、強靭な複合
プラスチックスを得ることが出来る。Normally, rope-like materials have air permeability and permeability, so the porosity is 3.
It is common knowledge that the properties of the material that makes up the rope, such as tensile strength, elongation, and flexural modulus, change significantly because it is more than 0%, and that some properties deteriorate by a factor of 50 or more. Therefore, a large reinforcing effect is achieved by forming small holes in a range where the characteristic values of the material of this rope-like material do not deteriorate to a level below that of Kano. That is, by punching small holes of 3.9 m or less in the reinforcing material so that the pore area per area is 20 or less, the reinforcing plastic penetrates the upper and lower parts of the reinforcing material and has a three-dimensional structure. As a result, strong composite plastics can be obtained.
ホ 本発明の効果
補強材の小孔を介し強化用プラスチックスで積層内部構
造が綱状又はラグ状を形成する為積層材料それぞれの伸
縮歪の差が小区画に独立した働きとなるのでトータルと
しての伸縮歪度を最小にすることが出来る。又強化用プ
ラスチックスと補強材の接触が恰もピン止めされた状態
となるので被強化プラスチックスのもつ引張強度が加算
されて接着強度が増加する。更に補強材の特性値の劣化
を極力低く押えるため金属材料を補強材とした場合より
金属性能に近い特性が得られる。且つ高価なカーボン・
金属・セラミック材などの繊維を用いる場合に比し本性
では1/10 以上のコストが合理化される。E. Effects of the present invention Since the inner structure of the laminate is formed into a rope-like or lug-like structure by reinforcing plastics through the small holes of the reinforcing material, the difference in expansion and contraction strain of each laminate material acts independently on the small sections, so the total The expansion and contraction distortion of can be minimized. Furthermore, since the reinforcing plastic and the reinforcing material are in a pinned state, the tensile strength of the reinforced plastic is added to increase the adhesive strength. Furthermore, since the deterioration of the characteristic values of the reinforcing material is kept as low as possible, properties closer to metal performance can be obtained than when a metallic material is used as the reinforcing material. And expensive carbon
Compared to the case of using fibers made of metal or ceramic materials, the cost is essentially 1/10 or more rationalized.
へ 本発明の説明
補強材としては気密なアルミ・鉄・ステンレス鋼・銅な
どの箔又は0.5−以下の薄板状ノモの或いはプラスチ
ックスのフィルム・シート状のものが用いられるが強化
用プラスチックスとの組合せにより、その応)14形態
は可変となる。即ち500℃以上の耐熱性をもつ金属材
料においては強化用プラスチックスとして熱硬化性会熱
可塑性のいずれの樹脂にも適用される。補強材として耐
熱度が金4類より低いプラスチックス類にあっては補強
用プラスチックスの耐熱度に応じ強化用プラスチックス
の拷類を撰択する必要がある。即ち200℃前後の耐熱
性をもつ補強用プラスチックスにあっては常温乃至10
0℃以下にて含浸可能の熱硬化樹脂又は重縮合性樹脂を
用いるなどである。Description of the present invention As a reinforcing material, an airtight foil of aluminum, iron, stainless steel, copper, etc., a thin plate with a thickness of 0.5 or less, or a plastic film or sheet is used, and reinforcing plastics are used. Depending on the combination with the base, the corresponding form can be changed. That is, for metal materials having heat resistance of 500° C. or higher, any thermosetting or thermoplastic resins can be used as reinforcing plastics. When using plastics as reinforcing materials whose heat resistance is lower than Class 4 metal, it is necessary to select the type of reinforcing plastic depending on the heat resistance of the reinforcing plastic. In other words, for reinforcing plastics that have a heat resistance of around 200°C, the temperature ranges from room temperature to 10°C.
For example, a thermosetting resin or a polycondensable resin that can be impregnated at 0° C. or lower is used.
従つてプラスチックス系補強材としては強化用プラスチ
ックスの浴融a度に対応したポリアミド・イミド、ポリ
イミド、ポリエーテAI ケ) :/ 、ポリフェニレ
ン0オキサイド、ポリフェニレンサルファイド、ポリア
セタール、ポリカーボネートなどの各111脂が、又強
化用プラスチックスとしてはポリオレフィン系スチレン
系を含めた熱可塑性樹脂及び熱硬化性、重縮合性樹脂を
それぞれ適応した組合せが可能となる。Therefore, as reinforcing materials for plastics, 111 resins such as polyamide/imide, polyimide, polyether AI, polyphenylene 0 oxide, polyphenylene sulfide, polyacetal, and polycarbonate, which correspond to the bath meltability of reinforcing plastics, are used. Furthermore, as the reinforcing plastics, suitable combinations of thermoplastic resins including polyolefin-based styrene-based resins, thermosetting resins, and polycondensation resins can be used.
搾孔法としては通常の打ち抜きき加工法でよいが金属箔
など無圧状態での搾孔を必要とする場合などでは電子線
又はレーザー光線による方法がすぐれている。孔径につ
いてはパンチ法により0.5m径(開孔率35俤以上)
の金属板が市場に出廻っているがこの孔径ともなれば樹
脂液の通過には加圧が必要となり、又孔径が大きくなる
と強化用樹脂面が強調されすぎることになるので孔径3
.0■以下が適当である。開孔率は強化材の特性と正相
関あり概ね特性値の20%低下は開孔率約2096以下
と推定されるのでこの範囲に設定するのが望ましい。A conventional punching method may be used as the hole punching method, but methods using electron beams or laser beams are superior in cases where hole punching is required under no pressure, such as in metal foils. The hole diameter is 0.5m by the punch method (open area ratio of 35 or more)
Metal plates with a diameter of 3 are on the market, but with this hole diameter, pressure is required for the resin liquid to pass through, and if the hole diameter becomes large, the reinforcing resin surface will be too emphasized, so the hole diameter of 3 is used.
.. A value of 0■ or less is appropriate. The porosity has a positive correlation with the properties of the reinforcing material, and it is estimated that a 20% decrease in the characteristic value is approximately 2096 or less in the porosity, so it is desirable to set it within this range.
実施例(1)
強化用プラスチックスとして市販の金属接着用の2液型
常温硬化のエポキシ樹脂を用いた。強化材として市販の
アルミ板(0,1m )の10cdのものを切り出し3
枚を用意しこれを重ねてその上に1 ’w方眼紙をおき
5.0+m間隔に打点して搾孔位置を定め2■の小孔を
ドリルにて搾孔した。この場合の開孔率は約12.5チ
であった。エポキシ混合物をアルミ箔の片面に塗付し2
枚目のアルミ箔にもエポキシ樹脂を塗り、2枚を重ねた
。3枚目も同様に繰返し1最後に表裏両面にもエポキシ
樹脂を塗り、テフロン・シート上に置き、上部に4.?
フロンシートを重ねて、軽く押え成形し反応を完了せし
め7層からなる厚み0.9mの積層品を得た。Example (1) A commercially available two-component room-temperature curing epoxy resin for metal bonding was used as the reinforcing plastic. Cut out a 10 cd piece of commercially available aluminum plate (0.1 m) as a reinforcing material 3
Two pieces of paper were prepared, stacked on top of each other, and a 1'w graph paper was placed on top of the paper, dots were dotted at intervals of 5.0+ m to determine the position for drilling, and 2 small holes were drilled using a drill. The porosity in this case was approximately 12.5 inches. Apply the epoxy mixture to one side of the aluminum foil 2
I also coated the second sheet of aluminum foil with epoxy resin and stacked the two sheets together. Repeat the same process for the third sheet. 1. Finally, apply epoxy resin to both the front and back sides, place it on a Teflon sheet, and apply 4. ?
The fluorocarbon sheets were stacked and lightly pressed to complete the reaction and a 7-layer laminate with a thickness of 0.9 m was obtained.
製品の断面はエポキシ樹脂を柱とする立体構造がルーパ
により確認された。搾孔しない比較品を同様手法で作製
し厚み0.75mのものなは2回目に早くもアルミ板と
の剥離がみられたが本性によるものは4回以上剥離しな
かった更にセラミック鋏で試験片を巾5m位いに切断し
たとき対象品の5■巾のものはアルき板が剥離するに対
し本性品では層間剥離がi!!!あら朴グいことによっ
ても確認出来た。The cross section of the product was confirmed to have a three-dimensional structure with epoxy resin as pillars using a looper. Comparison products without hole punching were made using the same method, and the one with a thickness of 0.75 m showed peeling from the aluminum plate as early as the second time, but the one due to its nature did not peel more than four times.Furthermore, it was tested with ceramic scissors. When a piece is cut to a width of about 5 m, the aluminum plate of the 5-cm-wide product in question peels off, but with the original product, interlayer peeling occurs. ! ! I was able to confirm this by doing some simple things.
実施例(2)
強化用プラスチックスとして熱可塑性ナイロン6(融点
225℃)の微粉末を用いた。Example (2) Fine powder of thermoplastic nylon 6 (melting point: 225° C.) was used as the reinforcing plastic.
補強材としてアルミ板(0,1wm )を用イ実施例(
1)に従い2枚を用意したがこの場合5■間隔に1.5
msの孔径で搾孔した。開孔率は約7係であった。テ
フロン・シート上にナイロン6粉末を薄((約1.0
m )広げアルミ板を置き、その上にナイロン6粉末を
同様に薄く広げ更にアルミ板を重ね最後にナイロン6を
薄く広げテフロン・シートで軽く押えて成形し約200
1の鉄板をおき加熱炉に入れ炉温220℃まで昇温し、
約2分後、加熱をやめ除冷した。5層からなる厚さ約2
.5謹の積層品を得た。Example using an aluminum plate (0.1wm) as a reinforcing material (
According to 1), two sheets were prepared, but in this case, 1.5 at 5 ■ intervals.
The holes were drilled with a hole diameter of ms. The open area ratio was approximately 7. Spread a thin layer of nylon 6 powder on a Teflon sheet (approximately 1.0
m) Place a spread aluminum plate, spread nylon 6 powder on top of it in the same way, and then layer the aluminum plate again.Finally, spread nylon 6 thinly and press it lightly with a Teflon sheet to form it.
Place the iron plate No. 1 in the heating furnace and raise the furnace temperature to 220℃.
After about 2 minutes, heating was stopped and the mixture was gradually cooled. Approximately 2 thick, consisting of 5 layers
.. A laminate product of 50% was obtained.
製品の断面はナイロン6樹脂を柱とする立体構造がルー
パにより確認されたが若干気泡が存在していた。工業的
には当然脱泡処理を考慮する必要がある。In the cross section of the product, a three-dimensional structure with nylon 6 resin as pillars was confirmed using a looper, but there were some air bubbles. Industrially, it is naturally necessary to consider defoaming treatment.
実施例(3)
強化用プラスチックスとして実施例(1)の市販エポキ
シ樹脂を用いた。補強材とし″″c25μmc25μm
ポリイミド用い実施例(1)に従い3枚を孔径2.5−
間隔5.0mに搾孔した。開孔率は約15.7%であっ
た。用意したポリイミド・フィルム上にエポキシ樹脂を
塗付し実施例(1)に従い7層の厚さ約0.7mの積層
品を得た。Example (3) The commercially available epoxy resin of Example (1) was used as the reinforcing plastic. As a reinforcing material ″″c25μmc25μm
According to Example (1) using polyimide, three sheets were made with a pore size of 2.5-
Holes were drilled at intervals of 5.0 m. The open area ratio was about 15.7%. An epoxy resin was applied onto the prepared polyimide film to obtain a 7-layer laminate with a thickness of about 0.7 m according to Example (1).
製品の断面はエポキシ樹脂を柱とする立体構造がルーパ
により確認された。The cross section of the product was confirmed to have a three-dimensional structure with epoxy resin as pillars using a looper.
Claims (2)
平板を補強材料とし、熱硬化性又は熱可塑性樹脂(以下
強化用プラスチックス)で積層板を製作するに当り、補
強材に多数の小孔(3.0mm孔径以下)を開孔率が1
.0〜20%となるよう搾孔することにより強化用プラ
スチックスを介し立体綱目状を構成する強化複合プラス
チックス。(1) When manufacturing a laminate using thermosetting or thermoplastic resin (hereinafter referred to as reinforcing plastics) using an airtight metal foil or metal film/sheet-like flat plate as the reinforcing material, many The opening rate of small holes (3.0 mm or less) is 1.
.. Reinforced composite plastics that forms a three-dimensional mesh shape through reinforcing plastics by drilling the holes to 0 to 20%.
スを用い、強化用プラスチックスとして熱硬化性樹脂を
用いる組合せで立体綱目状を構成する複合強化プラスチ
ックス。(2) A composite reinforced plastic that constitutes a three-dimensional mesh shape by using a plastic as a reinforcing material and a thermosetting resin as a reinforcing plastic as described in the preceding item 1.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP18156888A JPH0232840A (en) | 1988-07-22 | 1988-07-22 | Composite reinforced plastic prepared by laminating air-tight reinforcing material |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP18156888A JPH0232840A (en) | 1988-07-22 | 1988-07-22 | Composite reinforced plastic prepared by laminating air-tight reinforcing material |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0232840A true JPH0232840A (en) | 1990-02-02 |
Family
ID=16103079
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP18156888A Pending JPH0232840A (en) | 1988-07-22 | 1988-07-22 | Composite reinforced plastic prepared by laminating air-tight reinforcing material |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0232840A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2002081201A1 (en) * | 2001-04-03 | 2002-10-17 | Meng Chen | Decorative metal composite panal |
-
1988
- 1988-07-22 JP JP18156888A patent/JPH0232840A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2002081201A1 (en) * | 2001-04-03 | 2002-10-17 | Meng Chen | Decorative metal composite panal |
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