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JPH0346304B2 - - Google Patents
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JPH0346304B2 - - Google Patents

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Publication number
JPH0346304B2
JPH0346304B2 JP57130849A JP13084982A JPH0346304B2 JP H0346304 B2 JPH0346304 B2 JP H0346304B2 JP 57130849 A JP57130849 A JP 57130849A JP 13084982 A JP13084982 A JP 13084982A JP H0346304 B2 JPH0346304 B2 JP H0346304B2
Authority
JP
Japan
Prior art keywords
foam
axis
test
elongation
synthetic resin
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.)
Expired - Lifetime
Application number
JP57130849A
Other languages
Japanese (ja)
Other versions
JPS5920655A (en
Inventor
Hiroshi Tonokawa
Yasushi Ueda
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dow Kakoh KK
Original Assignee
Dow Kakoh KK
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 Dow Kakoh KK filed Critical Dow Kakoh KK
Priority to JP57130849A priority Critical patent/JPS5920655A/en
Publication of JPS5920655A publication Critical patent/JPS5920655A/en
Publication of JPH0346304B2 publication Critical patent/JPH0346304B2/ja
Granted legal-status Critical Current

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  • Laminated Bodies (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Molding Of Porous Articles (AREA)
  • Thermal Insulation (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

この発明はLNGあるいはLPG等の低温タンク
あるいはタンカーの断熱用として好適な低温断熱
用複合板に関する。その目的は極低温となして
も、クラツクの発生や、目地間が拡大せず寸法、
形状の安定性が高く、曲面にも添付けできる低
温、断熱用複合板を提案するにある。 従来、硬質ポリウレタン発泡体に合板等を積層
した複合板が低温用断熱材として用いられてい
た。ところが−100℃以下の極低温となると発泡
体が収縮し合板の木目に沿い目割れを生じ、これ
が内部の発泡体のクラツクを誘発させ、断熱性の
低下をもたらす欠点があつた。また、この欠点を
防止するために発泡体と合板との間に繊維層を介
装し合板の目割れを防止する提案(実開昭56−
110925号)もある。しかし、この方法によつても
発泡体内部の収縮応力の吸収が不充分で発泡体内
のクラツク発生を完全に防止することはできな
い。また、合板を積層した複合板は曲面とするこ
とが困難で、球形、筒形等の断熱面を形成できな
い欠点があつた。 この発明は上記問題点に着目してなされたもの
であり、その要旨は硬質合成樹脂発泡体の少なく
とも片表面に合板またはガラス繊維もしくは合成
繊維で補強された合成樹脂層を積層一体化して構
成してなり、該発泡体は密度が35〜100Kg/m3
厚さ方向をY軸、巾、長さ方向をX軸、Z軸とし
たときY軸方向の水蒸気透過率Py≦1.5〔g/m2
hr〕、X軸、Y軸方向の破断伸び率Ex、Eyが60
≧Ex≧8、60≧Ey≧8(%)の発泡体層が用け
てある低温断熱用複合板である。 この複合板は硬質合成樹脂発泡体を断熱層とす
るが、巾、長さ方向の伸度が8〜60%の高伸度の
発泡体層を設け積層板となして極低温となして
も、その収縮応力は高伸度発泡体層内で吸収緩和
しクラツクが発生しない、その収縮は積層した合
板またはガラス繊維もしくは合成繊維で補強され
た合成樹脂層の収縮能に拘束されて低減し被断熱
体の線膨張係数に近づくため敷設した場合目地が
開き難く、欠陥がない断熱層を形成できる。合成
樹脂層として反応型合成樹脂(例えばウレタン系
2液型接着剤)を発泡体に塗付して、押圧又は挟
持状態で形成、硬化を行うならば、円筒形、球面
形等の曲面にも成形でき、硬化した合成樹脂層の
剛性も加わつて、保形性も優れているので、曲面
の断熱が容易かつ確実となる。また同時に軽量で
ありながら圧縮強度が高く取付施工性が優れ、ク
リープ抵抗が高く長期高荷重の負荷に耐えること
ができるので、特にLNGタンク底部や側壁等大
面積の断熱層形成に好適である。 以下、この複合板を図面を用いて説明する。 第1図において、ポリスチレンからなる硬質合
成樹脂発泡体1(以下単に発泡体と略称する)の
片表面に合板またはガラス繊維もしくは合成繊維
で補強された合成樹脂層からなる層2(以下、表
面材という)が接着剤3を介して積層一体化し低
温断熱用複合板4(以下単に複合板と略称する)
が構成されている。 第2図においては、発泡体1の両表面に表面材
2,2を接着剤3,3を介して積層一体化し複合
板4が構成されている。 この2つの複合板4を構成する発泡体1は密度
が35〜100Kg/m3、厚み方向をY軸方向とした場
合、これに直交するX、Z軸方向の破断伸び率
Ex、Eyはそれぞれ、8%〜60%の範囲にあり、
Y軸方向の水蒸気透過率Py≦1.5〔g/m2・hr〕、
でなくてはならない。密度が35Kg/m3未満では低
温断熱用として充分な耐圧縮特性、耐クリープ
性、断熱性および耐透湿性を付与することができ
ない。100Kg/m3以上は剛性が高くなり、Ex、Ez
を8%以上とすることが困難となる。耐圧縮特性
から密度は40Kg/m3以上がより好ましい。水蒸気
透過率Pyは1.5以下である。長期的な断熱性能の
維持を重視するならばPyは1.0以下であれば一層
好適である。伸び率Ex、Ezは8〜60%である。
8%未満では低温時の収縮力の吸収緩和が不充分
であり、60%以上は水蒸気透過率や発泡体の機械
的性能の低下が大きくなり好ましくない。通常40
%以下の伸び率があればこの発明の目的を達成で
きる。表面材としては、5〜20mmの合板、ガラス
繊維又は合成繊維からなるネツト等で補強をされ
た合成樹脂(0.3〜2mm)等が使用でき、目的に
応じて選択される。発泡体と合板の接着剤として
は接着力と低温特性にすぐれるポリウレタン系、
エポキシ系等が用いられ、合成樹脂層も上記系統
の発泡体と接着力を有するものを用いるのがよ
い。 この複合板は以上の構成であり、第1図の複合
板4を発泡体1を断熱すべき低温物体に添付け、
あるいは第2図の複合板4を片面の表面材2を低
温物体に添付けて断熱施工される。複合板には、
低温物体側が低温で反対側が外気温度の温度勾配
が生じる。従つて低温側と高温側との間に収縮差
が生じ発泡体1層に歪応力が作用するが、この歪
応力はEx、Ezにより吸収緩和され、発泡体のク
ラツク発生が防止される。また同時に表面材との
界面剥離も起らない。 この複合板の表面材2に繊維補強樹脂等を用い
るならば、発泡体のX軸、Z軸共に高い伸び率を
有しているために例えば、第1図、第2図の複合
板を第3図、第4図のごとく断面円弧形の曲面と
なし、円筒形タンク等の断熱面が形成できるし、
第5図のごとく球殻形の曲面となし球形タンク等
の断熱面を形成できる。 第6図は、片面に補強表面材2を有し、発泡体
層が第1図の如く一層では、断熱性能が不足する
場合、複数層(発泡体層1a、1b)とした実施態
様を示したものである。被断熱体の温度と断熱材
の性能および要求される断熱条件に応じて、発泡
層を接着剤で積層一体化して厚い断熱層を形成で
きる。接着剤は、低温特性にすぐれた例えばウレ
タン系やエポキシ系のものが好ましい。各発泡体
層間には必要な応じ、ガラス繊維等メツシユを挿
入して接着層を補強して使うこともできる。 本発明でいう硬質合成樹脂発泡体とは、ポリス
チレン、メチルメタクリレート、塩化ビニル等で
代表される硬質合成樹脂を素材とする発泡体をい
う。 中でも発泡体そのものに圧縮強度及び長期の耐
圧縮クリープ性を要求したいときは、スチレン系
樹脂を用い、それを公知の押出発泡方法で発泡し
た発泡体を用いた方が有益である。 ポリエチレン系押出発泡体を構成するポリスチ
レンは、スチレンを主成分とする樹脂であるが、
スチレンの代わりa−メチルスチレン、ビニルト
ルエン、クロルスチレン等他のスチレン系モノマ
ーであつてもよい。 また上記スチレン系モノマーに共重合可能なモ
ノマー、例えばアクリロニトリル、メタクリロニ
トリル、アクリル酸メチル、メタクリル酸メチ
ル、無水マレイン酸、アクリルアミド、ビニルピ
リジン、アクリル酸、メタクリル酸等を共重合し
たコポリマーが含まれる。 更に上記スチルン系ポリマーにその特性が損わ
れない程度に他のポリマーをブレンドしたものも
差し支えない。 スチレンを主成分とするポリスチレン系押出発
泡体は、独立気泡に富み、断熱性、透湿抵抗、圧
縮強度、長期耐圧縮クリープにすぐれ、水蒸気透
過率も小さい特徴を有するが一般に破断伸び率は
5%以下であり、本発明の複合板に用いるために
は、Ex、Ez方向に8〜60%の伸度を付与しなく
ては、極低温下での熱応力を吸収したり、円筒形
や球面形状への成形が困難である。 本発明の複合板用の断熱板は以下の如く、X軸
(長さ方向)、Z軸(巾方向)に圧縮することによ
つて達成できる。 第7図に示すごとく2組の上下対をなす挟持駆
動レベル6,7及び8,9との間に、駆動速度差
を設け、この間に発泡体10を送り込み、その速
度差で搬送方向、例えばX軸方向に圧縮加工を施
こす。 駆動速度差と加工の回数により、8〜60%の伸
度を付与できる。同様にZ軸方向にも圧縮して大
きい伸度の発泡体を得る。 この伸度により、低温下における発泡層中に発
生する熱歪の吸収と被断熱体の形状にそつて円筒
又は球面形状に押圧成形が可能となる。 この複合板(第1及び2図)を円筒形あるい
は、球形の複合板として使用する場合の加工手段
につき以下に記載する。 表面材として、発泡体との接着性にすぐれ低温
の機械的特性のすぐれた反応型合成樹脂をガラス
繊維メツシユ補強したものを選択する。 第7図の装置で押圧加工した発泡体(条件例
示:ポリスチレン系)にウレタン系2液型接着剤
を全面に塗付して次いで、補強層を置き、その上
から同様の接着剤を塗付して上記補強層を埋め、
この補強接着層が未硬化の状態で、複合板を被断
熱体の曲率と同様の曲率の円筒あるいは球面形の
型表面に押圧あるいは挟持して60〜90℃が好まし
くは70℃〜80℃に加熱した条件で合成樹脂を硬化
完了させた後冷却して脱型する。 合成樹脂層の硬化条件によつては、これを冷間
で行ない曲面形成することもできる。しかし60〜
90℃に加熱する方が硬化時間も短かく、発泡体の
曲げ歪の緩和も完全に行われ、より好適である。 本発明でいう各特性の測定方法及び評価は、以
下のようにして行つた。 (1) 密度;〔Kg/m3〕 発泡体から5cm×5cm×5cmの立方体を採取
し、重量〔g〕、体積(cm3)から算出し、5個
の平均値を密度(Kg/m3)とする。 (2) 圧縮強度;〔Kg/m3〕 密度を測定した5cm×5cm×5cmの試験片の
厚さ方向(Y軸方向)で、ASTM D1621に基
づき圧縮強度を測定し5個の平均値で表す。 圧縮歪率は5%とする。但し5%以内に降伏
現象が発生する場合は、降伏値を圧縮強度と
し、以下の基準で評価する。
The present invention relates to a composite board for low-temperature insulation suitable for insulation of low-temperature tanks or tankers such as LNG or LPG. The purpose is to prevent cracks from occurring and the gap between joints to maintain dimensions even at extremely low temperatures.
We propose a low-temperature, heat-insulating composite board that has high shape stability and can be attached to curved surfaces. Conventionally, a composite board made by laminating plywood or the like on a rigid polyurethane foam has been used as a low-temperature heat insulating material. However, at extremely low temperatures below -100°C, the foam shrinks and cracks occur along the grain of the plywood, which causes cracks in the internal foam, resulting in a reduction in insulation. In addition, in order to prevent this drawback, a proposal was made to interpose a fiber layer between the foam and the plywood to prevent cracks in the plywood (1983-
110925) is also available. However, even with this method, the absorption of shrinkage stress within the foam is insufficient and the occurrence of cracks within the foam cannot be completely prevented. Moreover, it is difficult to form a curved surface of a composite board made by laminating plywood, and it has the disadvantage that it is not possible to form a heat-insulating surface in a spherical or cylindrical shape. This invention was made with attention to the above-mentioned problems, and its gist is that a synthetic resin layer reinforced with plywood, glass fiber, or synthetic fiber is laminated and integrated on at least one surface of a hard synthetic resin foam. The foam has a density of 35 to 100 Kg/m 3 ,
When the thickness direction is the Y axis, and the width and length directions are the X and Z axes, the water vapor permeability in the Y axis direction Py≦1.5 [g/m 2
hr], the elongation at break in the X-axis and Y-axis directions Ex and Ey are 60
This is a composite board for low temperature insulation using a foam layer with ≧Ex≧8 and 60≧Ey≧8 (%). This composite board uses a hard synthetic resin foam as a heat insulating layer, but it also has a high elongation foam layer with an elongation of 8 to 60% in the width and length directions. The shrinkage stress is absorbed and relaxed within the high elongation foam layer and no cracks occur, and the shrinkage is reduced by being constrained by the shrinkage ability of the laminated plywood or the synthetic resin layer reinforced with glass fiber or synthetic fiber. Since it approaches the coefficient of linear expansion of the heat insulating material, it is difficult for joints to open when it is laid, and a heat insulating layer without defects can be formed. If a reactive synthetic resin (for example, a two-component urethane adhesive) is applied to the foam as a synthetic resin layer and formed and cured by pressing or sandwiching, it can be applied to curved surfaces such as cylindrical and spherical shapes. It can be molded, and in addition to the rigidity of the hardened synthetic resin layer, it also has excellent shape retention, making it easy and reliable to insulate curved surfaces. At the same time, it is lightweight, has high compressive strength, is easy to install, has high creep resistance, and can withstand high loads over long periods of time, making it particularly suitable for forming heat insulating layers over large areas such as the bottoms and side walls of LNG tanks. This composite plate will be explained below using the drawings. In FIG. 1, a layer 2 (hereinafter referred to as surface material) made of a synthetic resin layer reinforced with plywood, glass fiber, or synthetic fiber is formed on one surface of a hard synthetic resin foam 1 (hereinafter simply referred to as foam) made of polystyrene. ) are laminated and integrated via an adhesive 3 to form a composite board for low-temperature insulation 4 (hereinafter simply referred to as composite board).
is configured. In FIG. 2, a composite plate 4 is constructed by laminating and integrating surface materials 2, 2 on both surfaces of a foam 1 via adhesives 3, 3. The foam 1 constituting these two composite plates 4 has a density of 35 to 100 kg/m 3 , and when the thickness direction is the Y-axis direction, the elongation at break in the X and Z-axis directions perpendicular to this is
Ex and Ey are each in the range of 8% to 60%,
Water vapor transmission rate in the Y-axis direction Py≦1.5 [g/m 2・hr],
Must be. If the density is less than 35 Kg/m 3 , sufficient compression resistance, creep resistance, heat insulation and moisture permeability cannot be imparted for low-temperature insulation. Rigidity is higher than 100Kg/ m3 , Ex, Ez
It becomes difficult to make it 8% or more. From the viewpoint of compression resistance, the density is more preferably 40 Kg/m 3 or more. Water vapor transmission rate Py is 1.5 or less. If maintaining long-term insulation performance is important, it is more suitable for Py to be 1.0 or less. The elongation rates Ex and Ez are 8 to 60%.
If it is less than 8%, the absorption and relaxation of shrinkage force at low temperatures will be insufficient, and if it is more than 60%, the water vapor permeability and mechanical performance of the foam will be significantly reduced, which is not preferable. Usually 40
The object of this invention can be achieved if the elongation rate is less than %. As the surface material, plywood with a thickness of 5 to 20 mm, synthetic resin (0.3 to 2 mm) reinforced with a net made of glass fiber or synthetic fiber, etc. can be used, and is selected depending on the purpose. Polyurethane-based adhesives with excellent adhesive strength and low-temperature properties are used as adhesives for foam and plywood.
Epoxy or the like is used, and the synthetic resin layer is preferably one that has adhesive strength with the above-mentioned foams. This composite plate has the above-mentioned structure, and the composite plate 4 shown in FIG. 1 is attached to a low-temperature object to insulate the foam 1.
Alternatively, the composite board 4 shown in FIG. 2 is heat-insulated by attaching the surface material 2 on one side to a low-temperature object. The composite board has
A temperature gradient occurs where the cold object side is cold and the opposite side is the outside temperature. Therefore, a shrinkage difference occurs between the low-temperature side and the high-temperature side, and strain stress acts on one layer of the foam, but this strain stress is absorbed and relaxed by Ex and Ez, thereby preventing the occurrence of cracks in the foam. At the same time, interfacial peeling with the surface material does not occur. If a fiber-reinforced resin or the like is used for the surface material 2 of this composite board, the composite board of FIGS. As shown in Figures 3 and 4, it can form a curved surface with an arcuate cross section, and can form an insulating surface for cylindrical tanks, etc.
As shown in FIG. 5, it is possible to form a curved surface in the shape of a spherical shell and a heat insulating surface for a spherical tank, etc. FIG. 6 shows an embodiment in which a reinforcing surface material 2 is provided on one side, and multiple layers (foam layers 1a and 1b) are used when the insulation performance is insufficient with a single foam layer as shown in FIG. It is something that Depending on the temperature of the object to be insulated, the performance of the insulation material, and the required insulation conditions, a thick insulation layer can be formed by laminating and integrating the foam layers with an adhesive. The adhesive is preferably a urethane-based or epoxy-based adhesive that has excellent low-temperature properties. If necessary, a mesh such as glass fiber may be inserted between each foam layer to reinforce the adhesive layer. The term "hard synthetic resin foam" as used in the present invention refers to a foam made of a hard synthetic resin such as polystyrene, methyl methacrylate, vinyl chloride, or the like. In particular, when compressive strength and long-term compression creep resistance are required of the foam itself, it is more beneficial to use a foam made by using a styrene resin and foaming it by a known extrusion foaming method. Polystyrene, which constitutes extruded polyethylene foam, is a resin whose main component is styrene.
Instead of styrene, other styrenic monomers such as a-methylstyrene, vinyltoluene, and chlorostyrene may be used. Also included are copolymers obtained by copolymerizing monomers copolymerizable with the above styrene monomers, such as acrylonitrile, methacrylonitrile, methyl acrylate, methyl methacrylate, maleic anhydride, acrylamide, vinylpyridine, acrylic acid, and methacrylic acid. . Furthermore, the above-mentioned styrene-based polymer may be blended with other polymers to the extent that its properties are not impaired. Extruded polystyrene foam, whose main component is styrene, is rich in closed cells and has excellent heat insulation, moisture permeation resistance, compressive strength, long-term compression creep resistance, and low water vapor permeability, but generally has a break elongation of 5. % or less, and in order to be used in the composite plate of the present invention, it is necessary to give it an elongation of 8 to 60% in the Ex and Ez directions, so that it can absorb thermal stress at extremely low temperatures and has a cylindrical shape or It is difficult to mold into a spherical shape. The heat insulating board for a composite board of the present invention can be achieved by compressing in the X axis (length direction) and Z axis (width direction) as described below. As shown in FIG. 7, a drive speed difference is provided between the two pairs of upper and lower clamping drive levels 6, 7 and 8, 9, and the foam 10 is fed between them, and the speed difference allows the transport direction to be adjusted, e.g. Perform compression processing in the X-axis direction. Depending on the drive speed difference and the number of processing operations, elongation of 8 to 60% can be imparted. Similarly, the foam is compressed in the Z-axis direction to obtain a foam with high elongation. This elongation makes it possible to absorb thermal strain generated in the foam layer at low temperatures and to press-form it into a cylindrical or spherical shape that conforms to the shape of the body to be insulated. Processing means for using this composite plate (FIGS. 1 and 2) as a cylindrical or spherical composite plate will be described below. As the surface material, a reactive synthetic resin with excellent adhesion to the foam and excellent mechanical properties at low temperatures is selected, reinforced with glass fiber mesh. A two-component urethane adhesive is applied to the entire surface of the foam (example of conditions: polystyrene type) that has been pressed using the device shown in Figure 7. Next, a reinforcing layer is placed, and the same adhesive is applied over it. and fill in the above reinforcing layer,
With this reinforcing adhesive layer in an uncured state, the composite board is pressed or clamped onto the surface of a cylindrical or spherical mold with a curvature similar to that of the object to be insulated to a temperature of 60 to 90°C, preferably 70 to 80°C. After curing the synthetic resin under heated conditions, it is cooled and removed from the mold. Depending on the curing conditions of the synthetic resin layer, this can be performed cold to form a curved surface. But 60~
Heating to 90°C is more preferable because the curing time is shorter and the bending strain of the foam is completely relaxed. The measurement method and evaluation of each characteristic referred to in the present invention were performed as follows. (1) Density; [Kg/m 3 ] Take a 5 cm x 5 cm x 5 cm cube from the foam, calculate it from the weight [g] and volume (cm 3 ), and calculate the average value of the 5 pieces as the density (Kg/m 3 ). 3 ). (2) Compressive strength; [Kg/m 3 ] The compressive strength was measured based on ASTM D1621 in the thickness direction (Y-axis direction) of the 5 cm x 5 cm x 5 cm test piece whose density was measured, and the average value of 5 pieces was calculated. represent. The compression strain rate is 5%. However, if a yield phenomenon occurs within 5%, the yield value is taken as the compressive strength and evaluated based on the following criteria.

【表】 (3) 破断伸び率〔%〕 引張強度測定法、ASTM D 1623 B法に
基づき指定の方向(X、及びZ)に、試験片を
引張り、破断した時の歪量(伸び量)〔mm〕を
測定し以下の式で計算し評価する。 試験片は各方向毎に合計5個を採取。 試験片;50mm×50mm×50mm 破断伸び率(Ex又はEz)=破断時
の伸び量〔mm〕/試験片の厚さ〔mm〕×100〔%〕 (4) 水蒸気透過率;WVTR〔g/m2・hr〕 25mm×80φの試験片3ケを採取し、ASTM
C 355に準じて測定する。25mm厚さでの
WVTRは次式で計算する。但し蒸留水を用い
る方法で行なう。 WVTR〔g/m2・hr〕=G/A・t G;重量変化〔g〕 t; 〃 Gの生じた時間巾(hr) A;透過面積(m2) (5) 熱伝導率の経時変化率 第8図に示すように押圧加工した製品を上部
より厚さ25mm、巾200mm、長さ200mmの試験片を
採取し、第9図に示す装置を用いて測定する。 断熱材12で囲んだ温度調節機13を備えた
容器11に27℃の水14を入れ、該容器の開口
部側を、前記の試料片15により、パツキン1
6を介して閉塞する。この際、試料片の下面と
容器内の水面との間は約30mmの距離を設けるよ
うに配置する。また、試験片15の上面は、循
環水口17及び18から循環される冷却水によ
つて2℃に冷却されている冷却板19に密着し
ている。このような状態を保つて14日間放置し
たのち、試料片の表面をガーゼで軽くふきと
り、ASTM C 518に従つてこのものの熱伝
導率λ′を測定し、あらかじめ試験前に同じ条件
下で測定した熱伝導率λとの変化の割合λ′/λ
を求め、次表に従つて評価する。
[Table] (3) Elongation at break [%] Amount of strain (amount of elongation) when a test piece is pulled in the specified directions (X and Z) and broken based on the tensile strength measurement method, ASTM D 1623 B method. Measure [mm] and calculate and evaluate using the following formula. A total of 5 test pieces were taken from each direction. Test piece; 50mm x 50mm x 50mm Elongation at break (Ex or Ez) = Elongation at break [mm] / Thickness of test piece [mm] x 100 [%] (4) Water vapor transmission rate; WVTR [g/ m 2・hr〕 Take 3 test pieces of 25mm x 80φ and ASTM
Measure according to C 355. At 25mm thickness
WVTR is calculated using the following formula. However, the method is to use distilled water. WVTR [g/m 2・hr] = G / A ・t G: Weight change [g] t: Time span during which G occurred (hr) A: Transmission area (m 2 ) (5) Thermal conductivity over time Rate of Change A test piece with a thickness of 25 mm, a width of 200 mm, and a length of 200 mm is taken from the top of the pressed product as shown in Figure 8, and measured using the apparatus shown in Figure 9. Water 14 at 27° C. is poured into a container 11 equipped with a temperature controller 13 surrounded by a heat insulating material 12, and the opening side of the container is covered with the gasket 1 using the sample piece 15.
occlude via 6. At this time, the sample piece is placed so that there is a distance of about 30 mm between the bottom surface of the sample and the water surface in the container. Further, the upper surface of the test piece 15 is in close contact with a cooling plate 19 that is cooled to 2° C. by cooling water circulated from circulation water ports 17 and 18. After being left in this condition for 14 days, the surface of the sample piece was wiped lightly with gauze, and the thermal conductivity λ' of this sample was measured in accordance with ASTM C 518, and was previously measured under the same conditions before the test. Rate of change from thermal conductivity λ λ′/λ
Calculate and evaluate according to the table below.

【表】 (6) パネル極低温抵抗性 50mm×300mm×300mmの試験板を採り、上下面
を切削仕上後、第10図のようにX軸、Z軸方
向を明示した試験発泡体21上下面に12mm×
300mm×300mmの合板(JAS規格品)23,24
をポリウレタン系2液型極低温用接着剤(住友
ベークライト社製:スミタツクEA90177)22
で接着し24時間×23℃の条件で0.5Kg/cm3の加
圧下で熟成硬化させて、試験用パネル20と
し、3枚を製作、試験する。 (1) 極低温:−160℃テスト 第11図に示すように上記試験用パネル2
0を−160℃±5℃に内部を温調した極低温
槽25の中に急激に入れ、5時間放置後常温
に急激に取り出し1時間放置する。この操作
を繰返し、4回行い、4回目に極低温槽25
から試験パネル20を取り出し直後試験発泡
板21の4つの面を観察しクラツクの有無と
発生した方向を確認する。1時間後に合板2
3,24、試験発泡板21の境界面にそつて
1コ歯型スライサーでスライスし、更に試験
発泡板21の内部に向つて約10mm厚さで5分
割したスライスサンプルを調整し、各々のス
ライスタンプル面に界面活性剤と着色用イン
クを混合した水を塗付し、サンプル表面のク
ラツクの有無と方向を調査記録する。 なお、極低温槽25内の温度コントロール
は、液体窒素ボンベ26から液体窒素配管2
7を介して槽内頂部の噴出ノズル29に導
き、ここで有孔ジヤマ板30に接触しながら
気化し、ガスは排出口32から出て槽内の温
度を下げる。液体窒素は槽内の温度計31と
タイマーを連動させたコントロール装置によ
り流量自動調節弁28の開閉で液体窒素流量
が調節される。 (2) 極低温:−196℃テスト 第12図に示すように、上記の試験用パネ
ル20を断熱材33で密閉された液体窒素浸
漬装置34で試験する。 ステンレス製の深底トレー35に液体窒素
36を液体窒素ボンベから直接、液体窒素配
管27と液体窒素導入弁37を介して導入
後、上記試験用パネル20を急激に液体窒素
36内に充分浸漬するように入れ、鉄製サポ
ート39の上にあらかじめ液体窒素中で冷却
済の鉄製重錘38をのせ、30分間連続浸漬し
た後、上記試験パネル20をふん囲気中に取
り出し、通風しながら1時間放置する。この
操作を4回行い、極低温−160℃のテストで
行つたと同様の装置と方法で発泡体外面、内
面のクラツクの有無と方向を調査記録する。 各々のテスト温度条件について、3ケの試
験パネルの調査記録の結果をもとに以下の基
準に従つて評価する。
[Table] (6) Panel cryogenic resistance A test plate of 50 mm x 300 mm x 300 mm was taken, and after cutting the top and bottom surfaces, the top and bottom surfaces of the test foam 21 with the X-axis and Z-axis directions clearly marked as shown in Figure 10. 12mm×
300mm x 300mm plywood (JAS standard product) 23, 24
Polyurethane-based two-component cryogenic adhesive (manufactured by Sumitomo Bakelite Co., Ltd.: Sumitaku EA90177) 22
The test panel 20 was prepared and three test panels were prepared and tested by adhering and aging and curing under a pressure of 0.5 Kg/cm 3 for 24 hours at 23°C. (1) Cryogenic temperature: -160℃ test As shown in Figure 11, the above test panel 2
0 is suddenly placed in a cryogenic chamber 25 whose internal temperature is controlled to -160°C±5°C, and after being left for 5 hours, it is quickly taken out to room temperature and left to stand for 1 hour. This operation is repeated 4 times, and the cryogenic chamber 25 is heated for the fourth time.
Immediately after taking out the test panel 20 from the test foam board 21, the four sides of the test foam board 21 are observed to confirm the presence or absence of cracks and the direction in which they occur. Plywood 2 after 1 hour
3, 24. Slice with a single-tooth slicer along the boundary surface of the test foam board 21, and further divide the sample into 5 slices with a thickness of about 10 mm toward the inside of the test foam board 21, and divide each slice into 5 slices. Water mixed with a surfactant and coloring ink is applied to the surface of the sample, and the presence or absence and direction of cracks on the sample surface are investigated and recorded. The temperature inside the cryogenic chamber 25 is controlled by connecting the liquid nitrogen cylinder 26 to the liquid nitrogen pipe 2.
7 to the jet nozzle 29 at the top of the tank, where it is vaporized while contacting the perforated barrier plate 30, and the gas exits from the outlet 32 to lower the temperature inside the tank. The flow rate of liquid nitrogen is adjusted by opening and closing an automatic flow rate control valve 28 by a control device in which a thermometer 31 in the tank and a timer are linked. (2) Cryogenic temperature: -196°C test As shown in FIG. 12, the test panel 20 described above is tested in a liquid nitrogen immersion device 34 sealed with a heat insulating material 33. After introducing liquid nitrogen 36 directly from the liquid nitrogen cylinder into the stainless steel deep-bottom tray 35 via the liquid nitrogen piping 27 and liquid nitrogen introduction valve 37, the test panel 20 is rapidly and sufficiently immersed in the liquid nitrogen 36. After placing the iron weight 38, which has been cooled in liquid nitrogen in advance, on the iron support 39 and immersing it continuously for 30 minutes, the test panel 20 is taken out into the atmosphere and left for 1 hour while being ventilated. . This operation was repeated four times, and the existence and direction of cracks on the outer and inner surfaces of the foam were investigated and recorded using the same equipment and method as used in the cryogenic -160°C test. Each test temperature condition will be evaluated according to the following criteria based on the results of the investigation records of the three test panels.

【表】【table】

【表】 (7) 耐クリーブ性 試験発泡体から50mm×50mm×50mmの試験片を
8ケ採取する。その中から5ケを選び、厚さ方
向(Y軸)の圧縮強度をASTM D 1621に従
つて測定し、平均圧縮強度(Kg/cm3)を求めこ
れをσcとする。残つた3ケをクリーブ測定用試
験片45とし、第13図に示すように厚さ方向
の上下面に厚さ5mmの合板41,42を接着剤
43,44を介して加圧接着硬化したものをク
リープ測定用複合体40とする。クリープ測定
用試験片45の厚さ方向(Y軸)の厚さを正確
に1/100mmの単位まで計測しこの寸法をT0とす
る。 第14図に示すようにクリーブ測定用複合体
40をクリープ測定装置46の重錘架台48と
装置架台50の間に静かにセツトし、次いで上
記で求めた平均圧縮強度σcの1/3の値σc/3か
ら求められる5×5×σc/3Kgから重錘架台
48の重量W1を差引いた重錘W2(W2=25×
σc/3−W1)を衝撃を与えぬように静かに載
荷する。載荷直後にダイヤルゲーザ47の目盛
をゼロにセツトする。23℃×1000時間経過後の
ダイヤルゲージ47の目盛T1すなわち1000時
間のクリープ量(mm)を1/100mm単位で読み取
り、以下の式に従つてクリープ量(%)を求
め、下記の基準で耐クリープ性を評価する。 クリープ量(%)=T1/T0×100
[Table] (7) Cleave resistance Take 8 test pieces of 50 mm x 50 mm x 50 mm from the test foam. Five pieces were selected from among them, and the compressive strength in the thickness direction (Y axis) was measured according to ASTM D 1621, and the average compressive strength (Kg/cm 3 ) was determined, and this was set as σ c . The remaining three specimens were used as test specimens 45 for cleave measurement, and as shown in FIG. 13, plywood boards 41 and 42 with a thickness of 5 mm were bonded and cured by pressure on the upper and lower surfaces in the thickness direction via adhesives 43 and 44. is defined as the creep measurement composite 40. The thickness of the test piece 45 for creep measurement in the thickness direction (Y axis) is accurately measured to the nearest 1/100 mm, and this dimension is defined as T 0 . As shown in FIG. 14, the cleave measurement complex 40 is gently set between the weight mount 48 of the creep measurement device 46 and the device mount 50, and then a value of 1/3 of the average compressive strength σc determined above is set. Weight W 2 (W 2 = 25 x
σc/3−W 1 ) is loaded gently to avoid shock. Immediately after loading, the scale of the dial gauge 47 is set to zero. After 1000 hours at 23°C, read the scale T1 of the dial gauge 47, that is, the creep amount (mm) for 1000 hours, in units of 1/100 mm, calculate the creep amount (%) according to the following formula, and calculate the creep amount (%) according to the following criteria. Evaluate creep resistance. Creep amount (%) = T 1 / T 0 ×100

【表】 実施例、比較例1 密度が35〜100Kg/m3、厚さ100mmのポリスチレ
ン押出発泡板(旭ダウ(株)社製;スタイロフオーム
)及びポリ塩化ビニル発泡板を第7図に示す押
圧装置で本文記載の製造方法に準じて、初めにX
軸方向(長さ方向)次いで、Z軸方向(巾方向)
に押圧加工した。この際第3表に示す押圧加工条
件の中、圧縮率と加工回数のみを適宜選択し、他
は同一条件で行い、高伸度を有する発泡板を作成
した。(実験No.1〜14) 比較のために、密度が28〜100Kg/m3のポリス
チレン押出発泡板(旭ダウ(株)社製;スタイロフオ
ーム 並びにポリ塩化ビニル発泡板の未加工のも
の及びX軸方向のみ加工したもの、X、Z軸共に
加工したものも作成した。 各々の発泡体について、本文記載の方法で、密
度X軸及びZ軸方向の破断伸び率、Y軸方向の水
蒸気透過率、熱伝導率の経時変化及び極低温抵抗
性(−160℃)に着目し、本文記載の方法と基準
で評価し、各々の結果とそれらを総合評価した結
果を第1表に示した。総合評価の基準は以下の行
つた。 ◎;すべての特性が○印のもの(最高水準を満た
すもの) ○;△印はあるが、○印が多いもの(本発明の目
的を満たすもの) ×;×印が1つでもあるもの(目的を達しないも
の) 第1表の結果によるとLNGタンク等の低温断
熱用発泡体は、硬質合成樹脂発泡体で密度が35〜
100Kg/m3、X軸、Z軸方向の破断伸び率が8〜
60%、Y軸方向の水蒸気透過率が1.5g/m2・hr
以下でなければならないとがわかる。
[Table] Example, Comparative Example 1 Figure 7 shows an extruded polystyrene foam board (manufactured by Asahi Dow Co., Ltd.; Styrofoam) and a polyvinyl chloride foam board with a density of 35 to 100 Kg/m 3 and a thickness of 100 mm. First, press X using a pressing device according to the manufacturing method described in the text.
Axial direction (length direction), then Z-axis direction (width direction)
Press-processed. At this time, among the pressing conditions shown in Table 3, only the compression ratio and the number of times of pressing were selected as appropriate, and the other conditions were the same, to create a foam board with high elongation. (Experiment Nos. 1 to 14) For comparison, extruded polystyrene foam boards with densities of 28 to 100 kg/m 3 (manufactured by Asahi Dow Co., Ltd.; Styrofoam, unprocessed polyvinyl chloride foam boards, and Those processed only in the axial direction and those processed in both the X and Z axes were also created.For each foam, the density, elongation at break in the X-axis and Z-axis directions, and water vapor permeability in the Y-axis direction were determined using the method described in the text. Focusing on changes in thermal conductivity over time and cryogenic resistance (-160°C), evaluations were made using the methods and criteria described in the text, and the results of each and the comprehensive evaluation are shown in Table 1.Overall The evaluation criteria were as follows: ◎; All characteristics marked with ○ (satisfied with the highest standards) ○: △ but with many ○ marks (satisfied with the purpose of the present invention) ×; Items with at least one x mark (items that do not achieve the purpose) According to the results in Table 1, low-temperature insulation foams for LNG tanks, etc. are hard synthetic resin foams with a density of 35~
100Kg/m 3 , elongation at break in X-axis and Z-axis directions is 8~
60%, water vapor transmission rate in the Y-axis direction is 1.5g/m 2・hr
It turns out that it has to be less than or equal to.

【表】 実施例、比較例2 この対比は、極低温下で高荷重の負荷が長期に
渉つてかかる場合の用途、例えばLLNG地下タン
ク内側断熱材の具備すべき特性を究明するという
観点からなされた実験例である。即ち、密度が35
〜100Kg/m3セルサイズ0.6〜0.1mm厚さ100mmとポ
リスチレン押出発泡板(旭ダウ(株)社製;スタイロ
フオーム )を第7図に示す押出装置で本文記載
の製造方法に準じて、初めにX軸方向(長さ方
向)次いでZ軸方向(巾方向)に押出加工した。
この際、第3表に示す押圧加工条件の中圧縮率と
加工回数のみを適宜選択し、他は同一条件で行
い、密度、圧縮強度、破断伸び率、水蒸気透過
率、熱伝導率の経時変化率、パネル極低温抵抗
性、耐クリープ性等の評価を行うための素材を作
成した。(実験No.15〜28) 比較のために、密度が28〜100Kg/m3のポリス
チレン押出発泡板(旭ダウ(株);スタイロフオーム
)の未加工のもの及びX軸方向のみ加工したも
の、X、Z軸共に加工したものも製造した。又発
泡体素材の比較のため、市販のポリスチレンビー
ズ発泡板、ポリ塩化ビニル押出発泡板及び成型板
(厚さ;20mm)ポリメチルメタクリル酸押出発泡
板(旭ダウ(株)試作品;厚さ20mm)の加工したもの
としないもの及び一般用硬質ポリウレタン(No.
47)LNG地下タンク断熱材料として処方された
半硬質ポリウレタン(No.48〜50)を加えて評価材
料とした。 各々の発泡体について、本文記載の方法で、密
度X軸及びZ軸方向の破断伸び率、Y軸方向の水
蒸気透過率、熱伝導率の経時変化、Y軸方向の圧
縮強度と耐クリープ性、及び極低温抵抗性(−
160℃と−196℃)に着目し、本文記載の方法と基
準で評価し、各々の結果とそれらを総合評価した
結果を第2表に示した。総合評価の基準は、以下
で行つた。 ◎;すべての特性が○印のもの(最高水準を満た
すもの) ○;△印はあるが、○印の多いもの(本発明の目
的を満たすもの) ×;×印が1つでもあるもの(目的を達しないも
の) 第2表の結果によると、本発明のLNG等のタ
ンクの内側断熱材用とする目的を満たす発泡体
は、ポリスチレン系押出発泡体で密度が35〜100
〔Kg/m3〕、X軸、Z軸方向の破断伸び率が8〜60
%、Y軸方向の水蒸気透過率が1.5〔g/m2・hr〕
以下でなければならないことが判る。更にLNG
地下タンクの断熱材としたの機能を高め、−196℃
の液体窒素の保冷材として考え他の特性も最高水
準にある本発明の発泡体では、密度が40〜100
〔Kg/m3〕、X軸及びZ軸方向の破断伸び率Ex、
Ezが12〜40%、Y軸方向の水蒸気透過率が1.0
〔g/m2・hr〕以下でなければならないことが判
る。
[Table] Example, Comparative Example 2 This comparison was made from the perspective of investigating the characteristics that the insulation material inside the LLNG underground tank should have in applications where high loads are applied for a long period of time at extremely low temperatures. This is an example of an experiment. That is, the density is 35
~100Kg/m 3 A polystyrene extruded foam board (manufactured by Asahi Dow Co., Ltd.; Styrofoam) with a cell size of 0.6 to 0.1mm and a thickness of 100mm was first prepared using the extrusion device shown in Figure 7 according to the manufacturing method described in the text. was extruded in the X-axis direction (length direction) and then in the Z-axis direction (width direction).
At this time, only the medium compression ratio and the number of pressing processing conditions shown in Table 3 were selected as appropriate, and the other conditions were the same, and changes over time in density, compressive strength, elongation at break, water vapor permeability, and thermal conductivity were performed. Materials were created for evaluation of panel resistance, cryogenic resistance, creep resistance, etc. (Experiment Nos. 15 to 28) For comparison, extruded polystyrene foam board (Asahi Dow Co., Ltd.; Styrofoam) with a density of 28 to 100 kg/m 3 was used, unprocessed and processed only in the X-axis direction. We also manufactured products that were machined on both the X and Z axes. In addition, for comparison of foam materials, commercially available polystyrene bead foam board, polyvinyl chloride extrusion foam board, molded board (thickness: 20 mm), and polymethyl methacrylic acid extrusion foam board (asahi Dow Co., Ltd. prototype; thickness 20 mm) were used. ) with and without processing, and general-purpose rigid polyurethane (No.
47) Semi-rigid polyurethane (No. 48-50) formulated as an LNG underground tank insulation material was added as an evaluation material. For each foam, the density at break elongation in the X- and Z-axis directions, the water vapor permeability in the Y-axis direction, the change in thermal conductivity over time, the compressive strength and creep resistance in the Y-axis direction, and and cryogenic resistance (−
(160°C and -196°C), the results were evaluated using the methods and criteria described in the text, and Table 2 shows the results for each and the overall evaluation. The criteria for the overall evaluation were as follows. ◎; All characteristics are marked with ○ (satisfying the highest standards) ○: There are △ marks, but there are many ○ marks (satisfying the purpose of the present invention) ×; Those with at least one × mark ( According to the results in Table 2, the foam that satisfies the purpose of being used as an internal insulation material for tanks such as LNG according to the present invention is extruded polystyrene foam with a density of 35 to 100.
[Kg/m 3 ], elongation at break in X-axis and Z-axis directions is 8 to 60
%, water vapor transmission rate in the Y-axis direction is 1.5 [g/m 2 hr]
It turns out that it must be less than or equal to. Furthermore, LNG
Enhances the function of underground tank insulation, allowing temperatures to reach -196℃
The foam of the present invention, which is considered as a cold insulator for liquid nitrogen and has other properties of the highest standard, has a density of 40 to 100.
[Kg/m 3 ], elongation at break in the X-axis and Z-axis directions Ex,
Ez is 12-40%, water vapor transmission rate in Y-axis direction is 1.0
It can be seen that it must be less than [g/m 2 hr].

【表】【table】

【表】 第3表 加工条件 加工までのエージング日数 :1日 加工厚さ :100mm 加工速度(入口ベルト) :12mm/sec 圧縮率(出入口ベルト速度比) :1.05〜1.33 押圧距離(入、出口ベルト軸間距離) :200mm 押圧固定時間 :3.6秒 加工回数 :1〜3回【table】 Table 3 Processing conditions Aging days until processing: 1 day Processing thickness: 100mm Processing speed (inlet belt): 12mm/sec Compression ratio (inlet/outlet belt speed ratio): 1.05 to 1.33 Pressing distance (distance between input and exit belt axes): 200mm Pressure fixing time: 3.6 seconds Number of processing: 1 to 3 times

【図面の簡単な説明】[Brief explanation of drawings]

第1図、第2図はそれぞれこの発明になる複合
板の断面図、第3図、第4図はそれぞれ第1図、
第2図の複合板を円筒形状に曲げ加工した状態の
斜視図、第5図は第1図の複合板を球面形状に曲
げ加工した状態の斜視図、第6図は第1図の複合
板において、断熱材の厚みを要求される場合、断
熱層を複数層に形成した実施態様を示す断面図、
第7図は発泡体を圧縮し高い伸び率を付与する状
態を示す模式図、第8図は熱伝導率の経時変化率
測定のためのサンプリング位置と寸法を示す図、
第9図は熱伝導率の経時変化特性を評価するため
の加速吸湿させるための装置の原理図、第10図
は極低温抵抗性評価用パネルを示す図、第11図
と第12図はパネルでの極低温抵抗性を評価する
ための装置の原理図で、第11図はマイナス160
℃のふん囲気でのテスト装置用、第12図は液体
窒素中への浸漬テスト装置を示す模式図、第13
図はクリープ量を測定するための複合体を示す
図、第14図はクリープ測定装置を示す模式図で
ある。 1……発泡体、2……表面材、3……接着剤、
4,4′……複合板、5……補強繊維層、6,7,
8,9……挟持駆動ベルト、10……発泡体、1
1……容器、12……断熱材、13……温度調節
器、14……水、15……試験片、16……パツ
キン、17,18……循環水出入口、19……冷
却板、20……極低温抵抗性試験パネル、21…
…試験発泡体、22……ウレタン系極低温用接着
剤、23,24……合板、25……極低温槽、2
6……液体窒素ボンベ、27……液体窒素配管、
28……液体窒素流量自動調節弁、29……液体
窒素噴出ノズル、30……有孔ジヤマ板、31…
…温度計、32……窒素ガス排出口、33……断
熱材、34……液体窒素浸漬試験装置、35……
深底トレイ、36……液体窒素、37……液体窒
素導入弁、38……鉄製重錘、39……鉄製サポ
ート、40……クリープ測定用複合体、41,4
2……合板、43,44……接着剤、45……ク
リープ測定用試験片、46……クリープ測定装
置、47……ダイヤルケージ、48……重錘架
台、49……重錘、50……クリープ測定装置架
台。
Figures 1 and 2 are cross-sectional views of the composite plate of the present invention, Figures 3 and 4 are Figure 1 and Figure 4, respectively.
Figure 2 is a perspective view of the composite plate shown in Figure 1 bent into a cylindrical shape, Figure 5 is a perspective view of the composite plate shown in Figure 1 bent into a spherical shape, and Figure 6 is the composite plate shown in Figure 1. , a cross-sectional view showing an embodiment in which the heat insulating layer is formed into multiple layers when the thickness of the heat insulating material is required,
Fig. 7 is a schematic diagram showing a state in which the foam is compressed and given a high elongation rate, Fig. 8 is a diagram showing sampling positions and dimensions for measuring the rate of change in thermal conductivity over time;
Figure 9 is a principle diagram of an apparatus for accelerated moisture absorption for evaluating the temporal change characteristics of thermal conductivity, Figure 10 is a diagram showing a panel for evaluating cryogenic resistance, and Figures 11 and 12 are panels. Figure 11 is a diagram of the principle of the device for evaluating cryogenic resistance at -160
12 is a schematic diagram showing a test device immersed in liquid nitrogen;
The figure shows a composite body for measuring the amount of creep, and FIG. 14 is a schematic diagram showing a creep measuring device. 1... Foam, 2... Surface material, 3... Adhesive,
4, 4'... Composite board, 5... Reinforcing fiber layer, 6, 7,
8, 9... Clipping drive belt, 10... Foam, 1
1... Container, 12... Insulating material, 13... Temperature controller, 14... Water, 15... Test piece, 16... Packing, 17, 18... Circulating water inlet/outlet, 19... Cooling plate, 20 ...Cryogenic resistance test panel, 21...
...Test foam, 22...Urethane cryogenic adhesive, 23, 24...Plywood, 25...Cryogenic tank, 2
6...Liquid nitrogen cylinder, 27...Liquid nitrogen piping,
28...Liquid nitrogen flow rate automatic control valve, 29...Liquid nitrogen jet nozzle, 30...Perforated jammer plate, 31...
...Thermometer, 32...Nitrogen gas outlet, 33...Insulation material, 34...Liquid nitrogen immersion test device, 35...
Deep tray, 36...Liquid nitrogen, 37...Liquid nitrogen introduction valve, 38...Iron weight, 39...Iron support, 40...Creep measurement complex, 41, 4
2... Plywood, 43, 44... Adhesive, 45... Test piece for creep measurement, 46... Creep measuring device, 47... Dial cage, 48... Weight mount, 49... Weight, 50... ...Creep measuring device mount.

Claims (1)

【特許請求の範囲】 1 硬質合成樹脂発泡体の少なくとも片表面に合
板またはガラス繊維もしくは合成繊維で補強され
た合成樹脂層を積層一体化して構成されてなり、
該発泡体は密度が35〜100Kg/m3厚さ方向をY軸、
巾、長さ方向をX、Z軸としたときY軸方向の水
蒸気透過率Py≦1.5〔g/m2・hr〕、X軸、Z軸方
向の破断伸び率Ex、Ezが60≧Ex≧8、60≧Ex
≧8(%)の発泡体層が設けてあることを特徴と
する低温断熱用複合板。
[Scope of Claims] 1. A synthetic resin layer reinforced with plywood, glass fiber, or synthetic fiber is laminated and integrated on at least one surface of a hard synthetic resin foam,
The foam has a density of 35 to 100 kg/ m3 , with the thickness direction being the Y axis,
When the width and length directions are the X and Z axes, the water vapor permeability in the Y-axis direction Py≦1.5 [g/m 2 hr], the elongation at break Ex and Ez in the X-axis and Z-axis directions is 60≧Ex≧ 8, 60≧Ex
A composite board for low-temperature insulation, characterized in that a foam layer of ≧8 (%) is provided.
JP57130849A 1982-07-27 1982-07-27 Composite board for low-temperature heat insulation Granted JPS5920655A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57130849A JPS5920655A (en) 1982-07-27 1982-07-27 Composite board for low-temperature heat insulation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57130849A JPS5920655A (en) 1982-07-27 1982-07-27 Composite board for low-temperature heat insulation

Publications (2)

Publication Number Publication Date
JPS5920655A JPS5920655A (en) 1984-02-02
JPH0346304B2 true JPH0346304B2 (en) 1991-07-15

Family

ID=15044124

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57130849A Granted JPS5920655A (en) 1982-07-27 1982-07-27 Composite board for low-temperature heat insulation

Country Status (1)

Country Link
JP (1) JPS5920655A (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07113068B2 (en) * 1989-12-11 1995-12-06 東レ株式会社 Fiber-reinforced foam and method for producing the same
JP2012132519A (en) * 2010-12-22 2012-07-12 Dow Kakoh Kk Pipe cover for pipe embedded in ground

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5912838A (en) * 1982-07-13 1984-01-23 ダウ化工株式会社 Composite board for low-temperature heat insulation

Also Published As

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