JPH0446348B2 - - Google Patents
Info
- Publication number
- JPH0446348B2 JPH0446348B2 JP60089253A JP8925385A JPH0446348B2 JP H0446348 B2 JPH0446348 B2 JP H0446348B2 JP 60089253 A JP60089253 A JP 60089253A JP 8925385 A JP8925385 A JP 8925385A JP H0446348 B2 JPH0446348 B2 JP H0446348B2
- Authority
- JP
- Japan
- Prior art keywords
- vacuum
- support material
- silica
- molded
- metal
- 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
Links
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 56
- 239000000463 material Substances 0.000 claims description 45
- 238000009413 insulation Methods 0.000 claims description 29
- 229910052751 metal Inorganic materials 0.000 claims description 28
- 239000002184 metal Substances 0.000 claims description 28
- 239000000377 silicon dioxide Substances 0.000 claims description 24
- 239000000835 fiber Substances 0.000 claims description 10
- 239000003995 emulsifying agent Substances 0.000 claims description 9
- 239000011882 ultra-fine particle Substances 0.000 claims description 9
- 230000002787 reinforcement Effects 0.000 claims description 6
- 238000002156 mixing Methods 0.000 claims description 5
- 238000000034 method Methods 0.000 description 14
- 239000000378 calcium silicate Substances 0.000 description 10
- 229910052918 calcium silicate Inorganic materials 0.000 description 10
- OYACROKNLOSFPA-UHFFFAOYSA-N calcium;dioxido(oxo)silane Chemical compound [Ca+2].[O-][Si]([O-])=O OYACROKNLOSFPA-UHFFFAOYSA-N 0.000 description 10
- 239000011148 porous material Substances 0.000 description 10
- 210000002268 wool Anatomy 0.000 description 10
- 230000006835 compression Effects 0.000 description 9
- 238000007906 compression Methods 0.000 description 9
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 6
- 230000000694 effects Effects 0.000 description 6
- 239000007789 gas Substances 0.000 description 6
- 239000000203 mixture Substances 0.000 description 6
- 239000002253 acid Substances 0.000 description 5
- 230000005855 radiation Effects 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 239000000843 powder Substances 0.000 description 4
- 230000002265 prevention Effects 0.000 description 4
- 238000007789 sealing Methods 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 3
- 239000013078 crystal Substances 0.000 description 3
- 239000002657 fibrous material Substances 0.000 description 3
- 210000001061 forehead Anatomy 0.000 description 3
- 239000011810 insulating material Substances 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 3
- 239000004115 Sodium Silicate Substances 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000011491 glass wool Substances 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 239000012774 insulation material Substances 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 229910052911 sodium silicate Inorganic materials 0.000 description 2
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 229910052915 alkaline earth metal silicate Inorganic materials 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 239000006229 carbon black Substances 0.000 description 1
- 239000004927 clay Substances 0.000 description 1
- NJLLQSBAHIKGKF-UHFFFAOYSA-N dipotassium dioxido(oxo)titanium Chemical compound [K+].[K+].[O-][Ti]([O-])=O NJLLQSBAHIKGKF-UHFFFAOYSA-N 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 229910010272 inorganic material Inorganic materials 0.000 description 1
- 239000011147 inorganic material Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000010451 perlite Substances 0.000 description 1
- 235000019362 perlite Nutrition 0.000 description 1
- 239000011164 primary particle Substances 0.000 description 1
- 239000012779 reinforcing material Substances 0.000 description 1
- 238000004826 seaming Methods 0.000 description 1
- -1 shirasu balloons Substances 0.000 description 1
- 150000004756 silanes Chemical class 0.000 description 1
- 125000005372 silanol group Chemical group 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000005979 thermal decomposition reaction Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
- 229910052845 zircon Inorganic materials 0.000 description 1
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Thermal Insulation (AREA)
- Refrigerator Housings (AREA)
- Laminated Bodies (AREA)
Description
【発明の詳細な説明】
産業上の利用分野
本発明は断熱性能にすぐれた真空断熱構造体に
関するものである。DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application The present invention relates to a vacuum insulation structure with excellent insulation performance.
従来の技術
一般に冷凍コンテナ、液化ガス貯槽等の高性能
の断熱を要する構造体では、断熱性能を向上させ
るために断熱壁を真空構造体にすることは良く知
られている。BACKGROUND ART Generally, in structures that require high-performance insulation, such as refrigerated containers and liquefied gas storage tanks, it is well known that the insulation walls are made into vacuum structures in order to improve the insulation performance.
しかるに断熱壁を真空構造体に形成する場合に
は、真空構造体を形成する内外壁(金属容器)に
真空荷重(1Kg/cm2)がかかり、このため、金属
容器には真空荷重に充分耐え得るよう肉厚材料を
使用することになる。しかしながら金属容器とし
て肉厚材料を使用すると、重量が重くなると共
に、加工に極めて多くの労力を費やすばかりか、
第2図に示すような厚肉材料で構成された真空断
熱構造体では、真空空間1を伝わる熱は少ないけ
れども、面部2aもしくは2bから、額部3aお
よび3bを伝わつて、面部2bもしくは2aに逃
げる熱が増大するという欠点があつた。このよう
なことから薄肉材料の金属容器を使用し得る真空
断熱構造体が種々開発されている。この種の真空
断熱構造体は、内外壁の間に真空荷重を受けるた
め、耐圧縮性の成形断熱材を支持材として装填す
るものであるが、耐圧縮性を満足するものは一般
に嵩比重が大きくなり、熱伝導度が大きくなり断
熱性能の点で問題があつた。 However, when forming an insulating wall in a vacuum structure, a vacuum load (1Kg/cm 2 ) is applied to the inner and outer walls (metal container) forming the vacuum structure, and therefore, the metal container cannot withstand the vacuum load sufficiently. You will need to use thicker material to obtain the desired results. However, if a thick material is used for the metal container, it will not only be heavy and require an extremely large amount of labor to process.
In the vacuum heat insulating structure constructed of thick material as shown in FIG. 2, although little heat is transmitted through the vacuum space 1, it is transmitted from the surface portion 2a or 2b, through the forehead portions 3a and 3b, and then to the surface portion 2b or 2a. The drawback was that the amount of heat escaping increased. For this reason, various vacuum insulation structures have been developed that can use thin-walled metal containers. This type of vacuum insulation structure receives a vacuum load between the inner and outer walls, so it is loaded with compression-resistant molded insulation material as a support material, but those that satisfy compression resistance generally have a bulk specific gravity. As the size increased, the thermal conductivity increased, causing problems in terms of insulation performance.
上述のような現状から、ケイ酸カルシウムのよ
うな連続開気孔構造を有する耐圧縮性、軽量の無
機質材料成形体を支持材として使用し、10-2torr
以下の真空断熱構造体が提案されている。 Due to the current situation as described above, compression-resistant, lightweight inorganic material moldings with a continuous open pore structure such as calcium silicate are used as supporting materials, and 10 -2 torr
The following vacuum insulation structures have been proposed.
この成形体は耐圧縮荷重が2Kg/cm2以上であ
り、しかも嵩比重が0.1g/c.c.程度と軽く、さら
に連続開気孔構造を有しているため、真空排気効
果も著しいものである。 This molded product has a compressive load resistance of 2 kg/cm 2 or more, a light bulk specific gravity of about 0.1 g/cc, and has a continuous open pore structure, so it has a remarkable vacuum evacuation effect.
発明が解決しようとする問題点
しかしながら、ケイ酸カルシウム成形体は、直
径数10μmのイガグリ結晶が成長して絡み合い数
10μm以下の比較的大きな空気孔を形成してなる
ものであるため、輻射防止能が小さく、また結晶
間の固体熱伝導、結晶と金属容器の間の熱伝導が
比較的大きく、10-2torr以下の真空下での熱伝導
度は、0.01Kcal/mh℃程度(常圧下では
0.03Kcal/mh℃)であり、比較的大きい。Problems to be Solved by the Invention However, in calcium silicate molded bodies, burr crystals with a diameter of several tens of micrometers grow and intertwine in number.
Because it has relatively large air holes of 10 μm or less, its radiation prevention ability is low, and solid heat conduction between crystals and heat conduction between crystals and metal containers are relatively large, resulting in a temperature of 10 -2 torr. The following thermal conductivity under vacuum is approximately 0.01Kcal/mh℃ (under normal pressure
0.03Kcal/mh℃), which is relatively large.
また熱伝導度の低い断熱材としては、パーライ
ト、シラスバルーン、ガラスバルーンのような微
小粉体(10-2torr以下の真空下での熱伝導度約
0.002Kcal/mh℃、但し常圧下では0.02Kcal/
mh℃)や、ガラスウール、シリカアルミナウー
ル、シリカウール、カーボンウール等の繊維状物
質(10-2torr以下の真空下での熱伝導度約
0.003Kcal/mh℃、但し常圧下では0.03Kcal/
mh℃)がある。しかし繊維状物質はもちろん真
空荷重に耐えられず、粉体の断熱材であつても、
バーライト等の粉体は独立気泡となつていて、ガ
スを内蔵しており、真空荷重を受けると気泡が破
壊して内蔵ガスを放出するため、荷重を受けるこ
とが不可能である。このため、真空下でこれらの
断熱材を使用する場合は、金属容器として肉厚材
料を使用することが必要となり、重量が重くなる
ことは必定である。 Insulating materials with low thermal conductivity include fine powders such as perlite, shirasu balloons, and glass balloons (thermal conductivity in a vacuum of 10 -2 torr or less).
0.002Kcal/mh℃, however, 0.02Kcal/mh under normal pressure
mh℃), fibrous materials such as glass wool, silica alumina wool, silica wool, and carbon wool (thermal conductivity in a vacuum of 10 -2 torr or less
0.003Kcal/mh℃, however, 0.03Kcal/mh under normal pressure
mh℃). However, fibrous materials cannot withstand vacuum loads, and even powder insulation materials cannot withstand vacuum loads.
Powder such as barlite has closed cells and contains gas, and when subjected to a vacuum load, the bubbles burst and release the built-in gas, making it impossible to bear the load. For this reason, when these heat insulating materials are used under vacuum, it is necessary to use a thick material for the metal container, which inevitably increases the weight.
本発明は、このような真空断熱構造体の欠点を
改良しようとするものであり、安価で断熱性能に
優れ、かつ真空排気操作が容易で軽量の真空断熱
構造体を提供することを目的とするものである。 The present invention aims to improve the drawbacks of such a vacuum insulation structure, and aims to provide a vacuum insulation structure that is inexpensive, has excellent insulation performance, is easy to perform evacuation operation, and is lightweight. It is something.
問題点を解決するための手段
上記問題点を解決するために本発明は、シラン
誘導体の熱処理または熱分解などの乾式法に比べ
て非常に安価な湿式法によつて得られる、一次粒
子径がサブミクロン以下の超微粒子シリカを主材
とし、これを繊維状物質と絡み合わせて成形し、
低熱伝導率の断熱材としたものを支持材として用
いるものである。Means for Solving the Problems In order to solve the above-mentioned problems, the present invention provides a method for reducing the primary particle size, which is obtained by a wet method which is much cheaper than a dry method such as heat treatment or thermal decomposition of a silane derivative. The main material is ultrafine silica particles of submicron size or less, which are intertwined with fibrous substances and molded.
A heat insulating material with low thermal conductivity is used as the supporting material.
すなわち、金属容器中に支持材を充填し、この
金属容器を密閉した後、この金属容器内を真空に
してなる真空断熱構造体において、前記支持材
を、ケイ酸ソーダを酸で分解する方法、アルカリ
土類金属ケイ酸塩を酸で分解する方法、あるいは
酸性白土を酸で分解する方法などの湿式法によつ
て得られる超微粒子シリカと繊維強化材を混合、
圧縮した成形体により構成したものである。 That is, in a vacuum insulation structure formed by filling a metal container with a support material, sealing the metal container, and then evacuating the interior of the metal container, a method of decomposing the support material with sodium silicate using an acid; Mixing ultrafine silica and fiber reinforcement obtained by wet methods such as decomposing alkaline earth metal silicate with acid or decomposing acid clay with acid,
It is constructed from a compressed molded body.
また、特に真空断熱構造体の内外壁間の温度差
が大きい場合は、前記超微粒子シリカと繊維強化
材に微小な乳化剤を混合し、圧縮成形して、これ
を支持材として用いることにより、輻射防止効果
を大きくするようにしたものである。 In addition, especially when the temperature difference between the inner and outer walls of the vacuum insulation structure is large, it is possible to mix a fine emulsifier with the ultrafine particle silica and fiber reinforcing material, compression mold it, and use it as a support material to radiate radiation. This is designed to increase the prevention effect.
作 用
シリカの超微粒子を多孔体に単独で成形するこ
とは困難である。またバインダーを用いて成形す
ると固体熱伝導が大きくなる。そこで超微粒子シ
リカと繊維状物質を高速で攪拌混合し、圧縮成形
することは良く知られている。Function It is difficult to mold ultrafine silica particles alone into a porous body. Furthermore, when molded using a binder, solid heat conduction increases. Therefore, it is well known that ultrafine silica particles and a fibrous material are stirred and mixed at high speed and compression molded.
この方法によれば、2Kg/cm2以上の圧縮強度を
持ち、かつサブミクロン以下の気孔を90%近く持
つ微小多孔体の支持材を得ることができる。 According to this method, a microporous support material having a compressive strength of 2 Kg/cm 2 or more and nearly 90% of submicron or smaller pores can be obtained.
この支持材は、粒子がサブミクロン以下である
ため、乳化剤を添加せず超微粒子シリカだけの場
合でも、ケイ酸カルシウム成形体にくらべて輻射
防止効果が大きい。内外壁間の温度差が大きい場
合は、本来の支持材の断熱性能、気孔の大きさに
影響を及ぼさない程度の粒径材質の乳化剤を混合
することによつて、一層輻射防止効果を向上させ
ることができる。 Since the particles of this support material are submicron or smaller, even when only ultrafine silica particles are used without adding an emulsifier, the radiation prevention effect is greater than that of a calcium silicate molded body. If the temperature difference between the inner and outer walls is large, the radiation prevention effect can be further improved by mixing an emulsifier with a particle size that does not affect the heat insulation performance of the original support material or the size of the pores. be able to.
またこの支持材は、粒子と粒子の点接触、粒子
と繊維の点接触で成形されているため、気孔率は
ケイ酸カルシウムの約95%にくらべて小さいが、
固体間の熱伝導は小さい。 In addition, because this support material is formed by point contact between particles and point contact between particles and fibers, the porosity is smaller than about 95% of calcium silicate.
Heat conduction between solids is small.
しかし、この支持材は常圧ではケイ酸カルシウ
ムと同様に5〜10%の水分を吸着するため、熱伝
導率は約0.03Kcal/mh℃とそれ程優れたもので
はないが、吸着水分の影響のない減圧下では、ケ
イ酸カルシウムよりはるかに優れた断熱性能を示
す。 However, like calcium silicate, this support material adsorbs 5 to 10% of water at normal pressure, so its thermal conductivity is not so good at about 0.03Kcal/mh℃, but it is less susceptible to the effects of adsorbed water. At no reduced pressure, it exhibits much better thermal insulation performance than calcium silicate.
一方、上記支持材は径がサブミクロン以下の連
続気孔で構成され、かつケイ酸カルシウム成形体
よりはるかに小さな気孔であり、したがつて真空
度を数Torr以下にすれば、空気の対流、空気分
子間の熱伝導はなくなる。 On the other hand, the above-mentioned supporting material is composed of continuous pores with a diameter of submicron or less, and the pores are much smaller than the calcium silicate molded body. Heat conduction between molecules disappears.
実施例
以下、本発明の実施例について具体的に説明す
る。Examples Examples of the present invention will be specifically described below.
本発明の支持材の主材として用いる超微粒子シ
リカは、ケイ酸ソーダを酸で分解して得られる非
晶質シリカのようなものであり、一般に湿式法超
微粒子シリカまたは湿式法ホワイトカーボンと呼
ばれており、例えば徳山曹達製Tokusil等があ
る。 The ultrafine particle silica used as the main material of the support material of the present invention is amorphous silica obtained by decomposing sodium silicate with acid, and is generally called wet process ultrafine particle silica or wet process white carbon. For example, there is Tokusil manufactured by Tokuyama Soda.
繊維強化材としては、シリカアルミナウール、
シリカウール、ガラスウール、アルミナフアイバ
ー等があるが、真空引き温度をなるべく高くで
き、かつ安価で繊維径が細いという理由で、シリ
カアルミナウールが好ましい。 As fiber reinforcement materials, silica alumina wool,
There are silica wool, glass wool, alumina fiber, etc., but silica alumina wool is preferred because it allows the evacuation temperature to be as high as possible, is inexpensive, and has a small fiber diameter.
乳化剤としては、基本的には3種の異なるタイ
プの一つであるか、またはその種のタイプの組み
合わせであつてもよい。これらの基本的タイプ
は、
(イ) 反射タイプ 例えば金属粉末類
(ロ) 散乱タイプ 例えば酸化チタン、ジルコン、
チタン酸カリウムウイスカー
(ハ) 吸収タイプ 例えばカーボンブラツク
である。 The emulsifier may basically be one of three different types or a combination of such types. These basic types are: (a) Reflective type, such as metal powder (b) Scattering type, such as titanium oxide, zircon, etc.
Potassium titanate whisker (c) Absorption type For example, carbon black.
湿式法超微粒子シリカと繊維強化材のみの場合
は、湿式法超微粒子シリカ93〜98重量部、繊維強
化材2〜7重量部を高速で攪拌混合し、成形型中
でプレス成形し、嵩密度0.22〜0.35Kg/m2(気孔
率83〜89%)の支持材とする。 In the case of using only wet process ultrafine particle silica and fiber reinforcement, 93 to 98 parts by weight of wet process ultrafine particle silica and 2 to 7 parts by weight of fiber reinforcement are stirred and mixed at high speed, press-molded in a mold, and the bulk density is determined. The supporting material should be 0.22 to 0.35 Kg/m 2 (porosity 83 to 89%).
一方、乳化剤を混合する場合は、超微粒子シリ
カ60〜75重量部、繊維強化材2〜7重量部、乳化
剤25〜40重量部を高速で攪拌混合し、成形型中で
プレス成形し、嵩密度0.29〜0.46Kg/m2(気孔率
83〜89%)の支持材とする。 On the other hand, when mixing an emulsifier, 60 to 75 parts by weight of ultrafine silica, 2 to 7 parts by weight of fiber reinforcement, and 25 to 40 parts by weight of emulsifier are stirred and mixed at high speed, press-molded in a mold, and the bulk density 0.29~0.46Kg/ m2 (porosity
83-89%) as a supporting material.
上記2種類の超微粒子シリカ成形体は、耐熱性
約850℃、常圧における熱伝導率0.025Kcal/mh
℃〜0.035Kcal/mh℃(50℃)、耐圧縮性2Kg/
cm2以上を有しており、また連続開気孔構造であ
る。 The above two types of ultrafine particle silica molded bodies have a heat resistance of approximately 850℃ and a thermal conductivity of 0.025Kcal/mh at normal pressure.
℃~0.035Kcal/mh℃(50℃), compression resistance 2Kg/
cm2 or more, and has a continuous open pore structure.
さて、超微粒子シリカ成形体は、上記のように
攪拌、混合、プレス成形して製造され、放出する
ガスは大気中から吸湿している水分のみである。
しかして上記のような超微粒子シリカ成形体を真
空断熱容器の支持材として使用する場合には、ま
ず、この所定形状の超微粒子シリカ成形体を加熱
炉で予め乾燥処理する。この超微粒子シリカ成形
体の乾燥条件は、通常約200℃で2時間程度保持
すればほぼ恒量となる。この処理によつて、シラ
ノール基は残るが、成形体内の吸着水分はほとん
ど確実に除去される。更に高温を採用すれば加熱
時間は格段に短縮される。 Now, the ultrafine silica molded body is produced by stirring, mixing, and press molding as described above, and the gas released is only moisture absorbed from the atmosphere.
When the ultrafine silica molded body as described above is used as a support material for a vacuum heat-insulated container, first, the ultrafine silica molded body having a predetermined shape is preliminarily dried in a heating furnace. The drying conditions for this ultrafine silica molded product are usually about 200° C. for about 2 hours, so that the weight becomes almost constant. Through this treatment, the silanol groups remain, but the moisture adsorbed within the molded article is almost certainly removed. Furthermore, if a high temperature is used, the heating time can be significantly shortened.
次いで第1図に示すような薄肉の金属面部11
a,11b、金属額部12a,12bで構成され
た容器に、予備加熱された上記支持材13を充填
する。前記金属面部11a,11bと金属額部1
2a,12bは、それぞれの端部において溶接ま
たは巻締めなどにより取り付けることによつて密
閉される。そして金属面部11bには封止弁14
を有する排気管15が埋め込み構造により取り付
けられている。 Next, a thin metal surface portion 11 as shown in FIG.
The preheated support material 13 is filled into a container composed of metal frames 12a and 12b. The metal surface parts 11a, 11b and the metal forehead part 1
2a and 12b are hermetically sealed by attaching them at their respective ends by welding or seaming. A sealing valve 14 is provided on the metal surface portion 11b.
An exhaust pipe 15 having a diameter is attached by an embedded structure.
この後、外部より100℃以上のなるべく高温で
加熱しながら短時間に真空引きする。この操作に
より、前記支持材13内の水分はほとんど放出さ
れ、さらに他の放出ガスも放出され、支持材13
内は高真空度に保持される。そして前記封止弁1
4を密閉することにより、金属容器内に支持材1
3が充填され、かつこの支持材13内が真空に保
持された真空断熱構造体が製造される。なお、こ
の場合、保持真空度1Torrで断熱性能は十分に
発揮できる。 After this, the chamber is heated from the outside at a temperature as high as 100°C or higher and evacuated for a short time. By this operation, most of the water in the support material 13 is released, and other gases are also released, and the support material 13 is released.
The inside is maintained at a high degree of vacuum. and the sealing valve 1
By sealing 4, the supporting material 1 is placed inside the metal container.
A vacuum insulation structure is manufactured in which the support material 13 is filled with the support material 13 and the inside thereof is maintained in a vacuum. In this case, the insulation performance can be sufficiently exhibited at a maintained vacuum level of 1 Torr.
次に本発明の二つの実施例について説明する。 Next, two embodiments of the present invention will be described.
実施例 1
次に示すような配合の原料を日本アイリツヒ(株)
製逆流式高速混合機を用い、5000r.p.mで混合し
た。Example 1 Raw materials with the following composition were produced by Nippon Airitzhi Co., Ltd.
The mixture was mixed at 5,000 rpm using a high-speed backflow mixer manufactured by Yamaha Motor Co., Ltd.
湿式法超微粒子シリカ(徳山曹達製Tokusil
P)
62重量部
酸化チタン (テグサ製Titanium Oxide P
−25)
33重量部
シリカアルミナウール(イビデン製イビウール
バルク)
5重量部
上記混合物を成形型に入れてプレス成形し、幅
1000mm、長さ2000mm、厚さ50mm、嵩密度0.31g/
cm3の支持材13とした。この支持材13は連続開
気孔構造で、耐圧縮性は2Kg/cm2以上を有してい
る。 Wet method ultrafine particle silica (Tokusil manufactured by Tokuyama Soda)
P) 62 parts by weight Titanium oxide (Titanium Oxide P manufactured by Tegusa)
-25) 33 parts by weight Silica alumina wool (IBIDEN's IBI WOOL bulk) 5 parts by weight The above mixture was put into a mold and press-molded, and the width
1000mm, length 2000mm, thickness 50mm, bulk density 0.31g/
The supporting material 13 was cm 3 . This support material 13 has a continuous open pore structure and has a compression resistance of 2 kg/cm 2 or more.
上記のように成形されたままの支持材13の常
圧における熱伝導率は0.030Kcal/mh℃(50℃)
であり、これはケイ酸カルシウム成形体に比べ特
に優れたものではない。これは大気中の水分を吸
湿しているためと思われる。しかし、水分の影響
のない真空中での熱伝導率は50℃で0.005Kcal/
mh℃、200℃でも0.008Kcal/mh℃と優れてい
る。 The thermal conductivity of the support material 13 as-formed as described above at normal pressure is 0.030 Kcal/mh℃ (50℃)
This is not particularly superior to calcium silicate molded bodies. This is thought to be because it absorbs moisture from the atmosphere. However, the thermal conductivity in a vacuum without the influence of moisture is 0.005 Kcal/at 50°C.
Excellent at 0.008Kcal/mh℃ even at mh℃ and 200℃.
そこで、支持材13をオーブンに入れ、200℃
で2時間加熱処理を行ない脱湿した。この支持材
13を厚み0.2mmのSUS304の金属面部11a,1
1bと厚み0.08mmのSUS304の金属額部12a,
12bで構成された容器に充填する。 Therefore, the supporting material 13 was placed in an oven at 200°C.
Heat treatment was performed for 2 hours to dehumidify. This supporting material 13 is connected to the metal surface portions 11a and 1 of SUS304 with a thickness of 0.2 mm.
1b and a metal frame part 12a of SUS304 with a thickness of 0.08mm,
12b is filled.
上記支持材13を充填した金属容器内は、100
℃以上の高温で短時間のうちに真空度1Torr以
下の真空断熱構造体とした。 The inside of the metal container filled with the support material 13 is 100
A vacuum insulation structure with a degree of vacuum of 1 Torr or less was created in a short time at a high temperature of ℃ or higher.
(実施例 2)
次に示すような配合の原料を実施例1と同様な
方法で混合した。(Example 2) Raw materials having the following composition were mixed in the same manner as in Example 1.
湿式法超微粒子シリカ(徳山曹達製Tokusil
P)
95重量部
シリカアルミナウール(イビデン製イビウール
バルク)
5重量部
上記混合物を成形型に入れてプレス成形し、幅
1000mm、長さ2000mm、厚さ50mm、嵩密度0.24g/
cm3の支持材13とした。この支持材13は連続開
気孔構造で、耐圧縮性は2Kg/cm2以上を有してい
る。 Wet method ultrafine particle silica (Tokusil manufactured by Tokuyama Soda)
P) 95 parts by weight Silica alumina wool (IBIDEN's IBI WOOL bulk) 5 parts by weight The above mixture was put into a mold and press-molded, and the width
1000mm, length 2000mm, thickness 50mm, bulk density 0.24g/
The supporting material 13 was cm 3 . This support material 13 has a continuous open pore structure and has a compression resistance of 2 kg/cm 2 or more.
上記のように成形されたままの支持材13の常
圧における熱伝導率は0.028Kcal/mh℃(50℃)
であり、水分の影響のない真空中での熱伝導率は
50℃で0.0045Kcal/mh℃、200℃では、
0.012Kcal/mh℃である。これらは、従来のケイ
酸カルシウム成形体にくらべ優れたものである
が、高温雰囲気で輻射の影響が大きくなると、乳
化剤を添加している実施例1よりも断熱性能は劣
る。 The thermal conductivity of the supporting material 13 as-formed as described above at normal pressure is 0.028 Kcal/mh℃ (50℃)
The thermal conductivity in vacuum without the influence of moisture is
0.0045Kcal/mh at 50℃, at 200℃,
0.012Kcal/mh℃. Although these are superior to conventional calcium silicate molded bodies, when the influence of radiation becomes large in a high-temperature atmosphere, the heat insulation performance is inferior to that of Example 1 in which an emulsifier is added.
成形した支持材13を実施例1と同様に、支持
材13を予備加熱して吸着水を放出させた後、厚
み0.2mmのSUS304の金属面部11a,11bと厚
み0.08mmのSUS304の金属額部12a,12bで
構成された容器に充填し、容器内を高温雰囲気で
短時間のうちに、真空度1Torr以下の真空断熱
構造体とした。 The molded support material 13 is preheated in the same manner as in Example 1 to release the adsorbed water, and then the metal face parts 11a and 11b of SUS304 with a thickness of 0.2 mm and the metal frame part of SUS304 with a thickness of 0.08 mm are formed. A container composed of 12a and 12b was filled with the mixture, and the inside of the container was kept in a high-temperature atmosphere for a short time to form a vacuum insulation structure with a degree of vacuum of 1 Torr or less.
実施例1、2共に支持材13の耐熱は約850℃
であるが、ステンレスの酸化着色を考慮すると、
250℃まではテンパーカラーもつくことなく使え
る。 The heat resistance of the support material 13 in both Examples 1 and 2 is approximately 850°C.
However, considering the oxidation coloration of stainless steel,
It can be used up to 250℃ without any temper color.
発明の効果
以上のように本発明によれば、低熱伝導率で耐
圧縮性に優れた超微粒子シリカ成形体を支持材と
しているため、薄肉の金属容器が使え、その結
果、軽量で断熱性能に優れた真空断熱構造体を得
ることができ、さらに本発明は超微粒子シリカと
して湿式法のものを使うため、安価な真空断熱構
造体が得られる。Effects of the Invention As described above, according to the present invention, since an ultrafine silica molded body with low thermal conductivity and excellent compression resistance is used as a support material, a thin metal container can be used, and as a result, it is lightweight and has high heat insulation performance. An excellent vacuum heat insulating structure can be obtained, and since the present invention uses wet method ultrafine silica particles, an inexpensive vacuum heat insulating structure can be obtained.
一方、従来のケイ酸カルシウム成形体を支持材
として使つた場合は、真空度が10-2torr以下必要
であるが、超微粒子シリカ成形体の気孔はサブミ
クロン以下であるため、1Torr以下でよく、一
層真空引き作業が容易である。また、真空度が小
さいため、金属容器からのガスの放出も少なく、
さらに超微粒子シリカのゲツター作用もあるた
め、極めて断熱性能の経年変化が少ないものであ
る。 On the other hand, when a conventional calcium silicate molded body is used as a support material, the degree of vacuum needs to be 10 -2 torr or less, but since the pores of the ultrafine silica molded body are submicron or less, a vacuum level of 1 Torr or less is sufficient. , vacuuming work is easier. In addition, because the degree of vacuum is low, there is less gas released from the metal container.
Furthermore, due to the getter action of ultrafine silica particles, there is extremely little change in thermal insulation performance over time.
さらに乳化剤を添加すれば、高温においても断
熱性能に優れた真空断熱構造体を提供できる。 Furthermore, by adding an emulsifier, it is possible to provide a vacuum insulation structure with excellent insulation performance even at high temperatures.
第1図は本発明の一実施例を示す真空断熱構造
体の断面図、第2図は従来の真空断熱構造体の断
面図である。
11a,11b……金属面部、12a,12b
……金属額部、13……支持材。
FIG. 1 is a sectional view of a vacuum insulation structure showing an embodiment of the present invention, and FIG. 2 is a sectional view of a conventional vacuum insulation structure. 11a, 11b...metal surface part, 12a, 12b
...Metal forehead part, 13...Supporting material.
Claims (1)
を密閉した後、この金属容器内を真空にしてなる
真空断熱構造体において、前記支持材を、湿式法
によつて得られる超微粒子シリカと繊維強化材を
混合、圧縮した成形体により構成した真空断熱構
造体。 2 支持材を乳化剤を含有する成形体により構成
した特許請求の範囲第1項記載の真空断熱構造
体。[Scope of Claims] 1. A vacuum insulation structure in which a metal container is filled with a support material, the metal container is sealed, and then the interior of the metal container is evacuated. A vacuum insulation structure made of a molded product obtained by mixing and compressing the resulting ultrafine particle silica and fiber reinforcement. 2. The vacuum heat insulating structure according to claim 1, wherein the support material is a molded body containing an emulsifier.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP60089253A JPS61250481A (en) | 1985-04-25 | 1985-04-25 | Vacuum insulation structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP60089253A JPS61250481A (en) | 1985-04-25 | 1985-04-25 | Vacuum insulation structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS61250481A JPS61250481A (en) | 1986-11-07 |
| JPH0446348B2 true JPH0446348B2 (en) | 1992-07-29 |
Family
ID=13965594
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP60089253A Granted JPS61250481A (en) | 1985-04-25 | 1985-04-25 | Vacuum insulation structure |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS61250481A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015182768A1 (en) * | 2014-05-30 | 2015-12-03 | 旭硝子株式会社 | Vacuum heat-insulating material |
-
1985
- 1985-04-25 JP JP60089253A patent/JPS61250481A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015182768A1 (en) * | 2014-05-30 | 2015-12-03 | 旭硝子株式会社 | Vacuum heat-insulating material |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS61250481A (en) | 1986-11-07 |
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