Patent Application
20230383894
The present disclosure relates to a thermal insulation sheet using a porous structure with low thermal conductivity.
Conventionally, various thermal insulation materials have been used for the purpose of heat flow control in in-vehicle parts, residential building materials, industrial equipment, and the like. In addition to high thermal insulation, thermal insulation materials are required to have various specifications according to their applications. For example, when a thermal insulation material is arranged around a member with a curved surface, such as a pipe, flexibility such as bendability is required so that the thermal insulation material can be arranged along the shape of the part. When the thermal insulation material is arranged in a limited narrow space inside a housing, thinness is required. In addition, in product transportation applications, relatively great flexibility is required such that the thermal insulation material can be folded or wound when packing a product.
A porous material such as silica aerogel is known as a material for the thermal insulation material. Silica aerogel has a pore structure that has a skeleton composed of a plurality of fine silica particles connected to each other and has a size of approximately 10 nm to 50 nm. The thermal insulation material using silica aerogel can be produced by coating a base material with a liquid composition having silica aerogel and a binder that connects silica aerogel and drying the liquid composition, as described in, for example, PCT Japanese Translation Patent Publication No. 2015-528071 (Patent Literature 1), Japanese Patent Laid-Open No. 2020-122544 (Patent Literature 2), and Japanese Patent Laid-Open No. 2020-139560 (Patent Literature 3).
Since the binder that connects silica aerogels together has higher thermal conductivity than silica aerogel, when the incorporated amount of the binder is large, thermal insulation is lower, which is disadvantageous. Therefore, in order to improve the thermal insulation, it is necessary to reduce the incorporated amount of the binder and increase the incorporated amount of silica aerogel as much as possible. However, in this case, a physical bonding force between silica aerogels is reduced, and thus the silica aerogels are likely to be separated from each other during deformation such as bending, and cracks are likely to occur.
For example, as described in Patent Literature 1, when a base material is made of a fibrous material such as a nonwoven fabric, the nonwoven fabric is impregnated with a liquid composition containing silica aerogel and a binder and cured. As a result, binding between silica aerogels is reinforced by fibers, which is desirable in terms of suppressing fall-off of silica aerogel and occurrence of cracks. However, as the nonwoven fabric is impregnated with the liquid composition and silica aerogel is supported on the fibers, rigidity of the thermal insulation material as a whole including the base material increases. As a result, the flexibility of the thermal insulation material is lowered, and it becomes difficult to apply the thermal insulation material in applications such as bending, winding, and packaging. In addition, when the base material is made of a fibrous material such as a nonwoven fabric, it is necessary to increase the thickness of the nonwoven fabric to some extent in order to suppress “show-through” in which the liquid composition seeps out to the opposite side through gaps between the fibers. Therefore, there is a limit to how thin the thermal insulation material can be when the base material is included. Incidentally, using a thermal insulation layer alone without a base material is not practical because the thermal insulation layer is fragile and has problems such as silica aerogel falling off. Moreover, when the incorporated amount of the binder is increased in order to suppress fall-off of silica aerogel, desired thermal insulation cannot be obtained.
Paragraph of Patent Literature 2 describes a sheet-like thermal insulation material having a total thickness of 5 mm, in which a polyethylene terephthalate (PET) film is used as a base material, and a thermal insulation layer containing silica aerogel is formed thereon. In Patent Literature 2, voids are actively created between silica aerogels, and a volume ratio of voids in the thermal insulation layer is 10% or more to 55% or less, thereby suppressing fall-off of silica aerogel and occurrence of cracks (fractures). Patent Literature 2 does not consider thinning of the thermal insulation material including the base material or improvement of flexibility.
Patent Literature 3 describes a thermal insulation material having a three-layer structure of “nonwoven fabric/thermal insulation layer containing silica aerogel/heat reflecting layer.” As the heat reflecting layer, an aluminum-deposited film or the like is described. In Patent Literature 3, the heat reflecting layer is added to the configuration of the nonwoven fabric and the thermal insulation layer to reflect the heat radiated from a heat source, thereby improving the thermal insulation. Patent Literature 3 does not consider thinning of the thermal insulation material or improvement of flexibility.
A thermal insulation sheet according to the present disclosure includes: a base material in the form of a sheet and having a thickness of 5 μm or more to 50 μm or less; and a thermal insulation layer arranged on at least one surface of the base material. The thermal insulation layer includes: a porous structure that has a skeleton composed of a plurality of particles connected to each other, has pores therein, and has a hydrophobic site at least on a surface out of the surface and inside of the porous structure; and a binder that connects the porous structures with each other and has an elongation at break of 200% or more.
The present disclosure provides a thermal insulation sheet that is thin and has excellent flexibility such as bendability.
According to the thermal insulation sheet of the present disclosure, the thickness of the base material is 5 μm or more to 50 μm or less. Therefore, the thermal insulation sheet can be thinned. Accordingly, the thermal insulation sheet of the present disclosure can be arranged in a narrow space, and is suitable for parts that require weight reduction and thinning. In addition, when the thickness of the thermal insulation sheet is reduced, the thermal insulation sheet becomes flexible, and thus the thermal insulation sheet can be easily folded or wound. For example, since many resin films are relatively inexpensive, the cost can be reduced by using a resin film as the base material. As described above, in a case where the base material is coated with a liquid composition having a porous structure and a binder and dried to produce a thermal insulation sheet, when a resin film is used as the base material, there are no voids inside the film, making it difficult for vapor to escape. Therefore, compared to the case of using a nonwoven fabric having voids between fibers, the coating film is less likely to dry. Accordingly, when the thickness of the resin film is large, the heating from the base material side is not sufficient, and there is a concern of the heat transfer in the coating film becoming uneven. When the coating film is not heated uniformly, the coating film may swell during drying, or the degree of drying may vary, which may cause cracks. Moreover, when the heating time is lengthened in order to sufficiently dry the coating film, the productivity is lowered. In this respect, according to the thermal insulation sheet of the present disclosure, the thickness of the base material is small, and thus the coating film is likely to be heated uniformly. Therefore, even if a resin film or the like is used as the base material instead of a nonwoven fabric, the thermal insulation sheet can be dried in a relatively short time, and problems during drying are less likely to occur.
According to the thermal insulation sheet of the present disclosure, the elongation at break of the binder that connects the porous structures with each other in the thermal insulation layer is 200% or more. By adopting a flexible binder with high elongation, the thermal insulation layer becomes flexible, and thus the thermal insulation sheet can be easily folded and wound. In addition, since the porous structures are less likely to separate from each other during deformation such as bending, the occurrence of cracks can be suppressed.
Hereinafter, embodiments of a thermal insulation sheet of the present disclosure will be described. In addition, the embodiments are not limited to the following embodiments, and can be implemented in various modifications and improvements that can be made by those skilled in the art.
A thermal insulation sheet of the present disclosure includes a base material and a thermal insulation layer.
The base material is in the form of a sheet and has a thickness of 5 μm or more to 50 μm or less. The thickness of the base material is desirably 10 μm or more from the viewpoint of strength, and desirably 30 μm or less from the viewpoint of flexibility. The base material may consist of a single layer, or may be a laminate in which two or more layers of the same material or different materials are laminated. In order to arrange the thermal insulation sheet along the shape of a part, the base material must have flexibility such as bendability. However, from the viewpoint of suppressing excessive elongation of the thermal insulation layer during deformation and suppressing the occurrence of cracks, the elongation at break of the base material is desirably 150% or less.
As the base material, a resin film such as PET, polyimide, polyamide, polyphenylene sulfide (PPS), polyethylene naphthalate (PEN), and polyethylene (PE); a cellophane film made from pulp; and a metal film such as aluminum, an aluminum compound, magnesium, a magnesium compound, stainless steel, silver, titanium, a titanium compound, and tin are suitable. In addition, a metal-deposited film obtained by depositing a metal on the surface of a resin film by vacuum deposition or sputtering is also suitable. Examples of the metal-deposited film include an aluminum-deposited film and a titanium-deposited film. When the base material has a metal layer (vapor-deposited film) and a resin layer (resin film), such as a metal-deposited film, and the thermal insulation layer is arranged on one side of the base material, it may be appropriately determined on which of the metal layer or the resin layer the thermal insulation layer should be arranged in consideration of the usage pattern of the thermal insulation sheet. The metal-deposited film may be a film having a three-layer structure in which a deposited film is further coated with a resin layer from the viewpoint of corrosion suppression and protection of the deposited film. In order to improve the adhesiveness between the base material and the thermal insulation layer, the surface of the base material may be subjected to pretreatment such as a coupling treatment.
A thermal insulation layer is arranged on at least one surface of the base material. The thermal insulation layer may be arranged only on one side of the base material, or may be arranged on both sides. The thickness of the thermal insulation layer is desirably 0.2 mm or more, 0.3 mm or more, or 0.5 mm or more from the viewpoint of ensuring desired thermal insulation. From the viewpoint of flexibility and thinning, the thickness is desirably 1.2 mm or less, 1 mm or less, or 0.7 mm or less. The thermal insulation layer has a porous structure and a binder that connects the porous structures with each other.
The porous structure has a skeleton composed of a plurality of particles connected to each other, and has pores therein. It is desirable that the diameter of the particles (primary particles) forming the skeleton be approximately 2 nm to 5 nm, and the size of the pores formed between the skeletons be approximately 10 nm to 50 nm. Many of the pores are so-called mesopores of nm or less. Since mesopores are smaller than the mean free path of air, air convection is suppressed and heat transfer is inhibited. The shape of the porous structure is not particularly limited, and may be a spherical shape, an irregularly shaped lump shape, or the like, but a chamfered shape or a spherical shape is desirable. In this case, since dispersibility in the liquid is improved, preparation of the composition (thermal insulation layer coating material) for producing the thermal insulation layer is facilitated. In addition, it is possible to increase the filling amount by reducing voids between the porous structures, and to improve the thermal insulation. The porous structure may be used in a produced state, or may be used after being further pulverized. For a pulverizing treatment, a pulverizing device such as a jet mill or a spheroidizing device may be used. By performing the pulverizing treatment, corners of the particles are removed and the particles have a rounded shape. Accordingly, binding is likely to be performed by the binder, and the porous structure is less likely to fall off. In addition, the surface of the thermal insulation layer becomes smooth and cracks are less likely to occur.
The particle size of the porous structure may be relatively small and uniform from the viewpoint of forming a thin thermal insulation layer and smoothing the surface such that cracks are less likely to occur. For example, it is desirable to use a porous structure having a 90% diameter (D90) of 150 μm or less in a particle size distribution. The particle size of the porous structure may be adjusted by removing large particles by a classification treatment such as sieving.
Porous structures include hydrophilic ones having a hydrophilic site on the surface and inside, and hydrophobic ones having a hydrophobic site. Among these, the hydrophilic porous structure is fragile and easily crumbles. In addition, there is a concern of moisture or the like entering and the pores being crushed. Therefore, in the thermal insulation sheet of the present disclosure, a hydrophobic porous structure having a hydrophobic site at least on the surface out of the surface and the inside thereof is used. When a hydrophobic porous structure is used, in a case where an aqueous binder in which water is used as a solvent is used, the binder is less likely to enter the pores of the porous structure, and thus the thermal insulation is less likely to be inhibited. In addition, the surface of the porous structure may be surface-treated with a silane coupling agent or the like. By performing the surface treatment, functions such as hydrophobicity can be imparted to the surface of the porous structure.
The type of the porous structure is not particularly limited. Examples of primary particles include silica, alumina, zirconia, and titania. Among them, from the viewpoint of excellent chemical stability, silica aerogel in which the primary particles are silica, that is, silica aerogel which has a skeleton composed of a plurality of fine silica particles connected to each other, is desirable. Silica aerogel is white and reflects infrared rays. Therefore, when silica aerogel is used, a heat shielding effect can be imparted to the thermal insulation layer.
The method for producing silica aerogel is not particularly limited, and the drying process may be performed at normal pressure or may be performed under supercritical conditions. For example, when the hydrophobization treatment is performed before the drying process, the need for supercritical drying is eliminated, that is, the drying may be performed at normal pressure, and thus production can be performed more easily at a low cost. Due to the difference in drying method when producing aerogel, the one dried at normal pressure may be called “xerogel,” and the one dried under supercritical conditions may be called “aerogel,” but both are referred to as “aerogels” in the present specification.
The content of the porous structure in the thermal insulation layer may be appropriately determined in consideration of thermal insulation, flexibility, mechanical strength, and the like. For example, from the viewpoint of reducing thermal conductivity (increasing thermal insulation), the content of the porous structure is desirably 80% by volume or more when the volume of the entire thermal insulation layer is 100% by volume. More preferably, the content of the porous structure is 85% by volume or more. On the other hand, when the number of porous structures is increased, the content of the binder correspondingly decreases, and thus there is concern of the flexibility decreasing or the porous structure becoming likely to fall off. Therefore, the content of the porous structure is desirably 96% by volume or less when the volume of the entire thermal insulation layer is 100% by volume. The content of the porous structure is more preferably 92% by volume or less.
As the binder, one having an elongation at break of 200% or more is used. When the elongation at break is less than 200%, the flexibility of the thermal insulation layer is reduced, and thus cracks are likely to occur during deformation such as bending. The elongation at break of the binder may be measured by a method conforming to JIS K6251:2017. Dumbbell No. 3 (parallel portion thickness 2.0 mm) is used as a test piece. In addition, from the viewpoint of suppressing excessive elongation of the thermal insulation layer during deformation to suppress the occurrence of cracks, the ratio (E2/E1) of the elongation at break (E2) of the binder to the elongation at break (E1) of the base material is desirably 1.33 or more to 30 or less. The elongation at break of the base material may be measured by the same method as for the binder, but the test piece is Dumbbell No. 3 having the same thickness as the base material.
As the binder, it is desirable to use a binder (aqueous binder) which has one or more selected from resin and rubber and uses water (including pure water, tap water, and the like) as a solvent. Examples of the aqueous binder include a water-soluble binder and an emulsion-like binders, and among them, the emulsion-like binder (aqueous emulsion binder) is suitable. The aqueous emulsion binder is emulsified by introducing a surfactant or a hydrophilic group. According to the aqueous emulsion binder, the surfactant and the hydrophilic group volatilize during drying, and accordingly, hydrophilicity is lowered and the water is less likely to be dissolved. Therefore, it is considered that less stickiness occurs after the thermal insulation layer coating material is cured. The emulsification method may be a forced emulsification type using a surfactant as an emulsifier or a self-emulsification type in which a hydrophilic group is introduced.
The glass transition temperature (Tg) of the binder is desirably −5° C. or lower, more desirably −20° C. or lower, from the viewpoint of having high adhesiveness to the porous structure and softening the thermal insulation layer to make cracks less likely to occur. For example, in the case of an aqueous emulsion binder, a resin emulsion or a rubber emulsion may be employed. Examples of the resin include acrylic resin, urethane resin, and a mixture of acrylic resin and urethane resin. Examples of the rubber include styrene-butadiene rubber (SBR), nitrile rubber, silicone rubber, urethane rubber, and acrylic rubber. Urethane resin, styrene-butadiene rubber, and the like are suitable from the viewpoint of making the thermal insulation layer flexible. From the viewpoint of improving the heat resistance of the thermal insulation layer, an acrylic resin or the like is suitable. From the viewpoint of increasing the strength of the binder portion and improving the strength of the thermal insulation layer, a crosslinking agent or the like may be used in combination to crosslink the binder component.
In addition to the porous structure and the binder, the thermal insulation layer may contain other components such as a crosslinking agent, a thickener, a reinforcing fiber, a flame retardant, and the like. A porous structure having a hydrophobic site on the surface or inside is less likely to be compatible with water. Among them, silica aerogel has a low specific gravity, and thus silica aerogel is likely to float on water. Therefore, it is difficult to disperse silica aerogel in a binder liquid using water as a solvent, and the dispersing process takes time. For example, when a thickener is incorporated, the viscosity of the binder liquid increases, and the porous structure is likely to disperse. Thereby, the time required for dispersing the porous structure can be shortened, and the productivity can be improved. In addition, since flexibility is imparted to the thermal insulation layer, the occurrence of cracks is also suppressed. As the thickener, polysaccharides such as carboxymethyl cellulose (CMC), carboxyethyl cellulose, carboxypropyl cellulose, hydroxyethyl cellulose, hydroxypropyl cellulose, xanthan gum, agarose, and carrageenan; polyvinyl alcohol; polyethylene oxide; glucomannan, and the like may be used.
When the reinforcing fiber is incorporated, the reinforcing fiber is physically entangled around the porous structure, and accordingly, it is possible to improve the mechanical strength of the thermal insulation layer, and to suppress fall-off of the porous structure. Although the type of the reinforcing fiber is not particularly limited, a ceramic fiber such as glass fiber and alumina fiber is suitable in consideration of heat resistance.
When a flame retardant is incorporated, flame retardancy can be imparted to the thermal insulation layer. A halogen-based, phosphorus-based, metal hydroxide-based, and other known flame retardant may be used as the flame retardant. Considering the environmental load, it is desirable to use a phosphorus-based flame retardant. Examples of the phosphorus-based flame retardant include ammonium polyphosphate, red phosphorus, and a phosphate ester. Among them, a water-insoluble one is desirable, and for example, ammonium polyphosphate is preferable, because the flame retardant is less likely to flow out even when the flame retardant comes into contact with moisture during use.
The thermal insulation sheet of the present disclosure can be produced by coating the base material with the thermal insulation layer coating material and drying the same. The thermal insulation layer coating material may be prepared by incorporating the porous structure, the binder, and components added as necessary, and stirring the mixture. When the binder does not contain water, the thermal insulation layer coating material may be prepared by adding water as appropriate. When the porous structure is silica aerogel, considering the dispersibility thereof, it is desirable to add a thickener to a binder or a liquid in which a binder is added to water to increase the viscosity of the liquid, and then add silica aerogel. The stirring may be blade stirring, or positive shearing force or ultrasonic waves may be applied. A rotation/revolution stirring device or a media type stirring device may be used.
For coating the thermal insulation layer coating material, brush coating, a coating machine such as a blade coater, a bar coater, a die coater, a comma coater (registered trademark), or a roll coater, or a sprayer may be used. After coating, the coating film may be dried and cured by holding the coating film at a temperature of 80° C. to 150° C. for approximately 0.5 minute to several minutes. For example, when adopting a roll-to-roll method, productivity is improved.
Next, the present disclosure will be described more specifically with reference to Examples.
First, silica aerogel (having an average particle size of 90 μm) having a hydrophobic site on the surface and the inside thereof was pulverized into spheres. The pulverization treatment was performed for 10 minutes at a rotation speed of 4000 rpm using a collision disperser. The pulverized silica aerogel was sieved using a sieve with an opening of 106 μm to remove large particles. When the particle size distribution of silica aerogel after sieving was measured, the 90% diameter (D90) was 92 μm.
Next, a urethane resin composition (“Evaphanol (registered trademark) HA-55” produced by Nicca Chemical Co., Ltd.) was added to water as an aqueous emulsion binder, and silica aerogel of which the particle size was adjusted was added while stirring with a stirring blade. In this state, stirring was continued for 30 minutes at a rotation speed of 1000 rpm, and then the mixture was allowed to stand for 60 minutes to produce a thermal insulation layer coating material. The binder used has a Tg of −30° C. and an elongation at break of 430%.
Subsequently, the produced thermal insulation layer coating material was applied to coat a PET film (“Lumirror (registered trademark) #12” produced by Toray Industries, Inc., having a thickness of 12 μm and an elongation at break of 140%) as a base material using a roll coater. Then, the thermal insulation layer coating material was dried at 150° C. for 1 minute to produce a thermal insulation sheet having a thermal insulation layer thickness of 0.3 mm.
The content of silica aerogel in the thermal insulation layer is 90% by volume when the entire thermal insulation layer is 100% by volume. The ratio of the elongation at break (E2) of the binder to the elongation at break (E1) of the base material (E2/E1, hereinafter referred to as the “elongation ratio of the binder to the base material”) is 3.1. In addition, the elongation at break of the base material shown in the present example is all elongation in the film molding direction (MD). The produced thermal insulation sheet is called the thermal insulation sheet of Example 1.
A thermal insulation sheet of Example 2 was produced in the same manner as in Example 1, except that the thickness of the thermal insulation layer was changed to 1 mm.
A thermal insulation sheet of Example 3 was produced in the same manner as in Example 1, except that the thickness of the base material was changed. A PET film having a thickness of 50 μm (“Lumirror #50” produced by Toray Industries, Inc., having an elongation at break of 150%) was used as the base material. The elongation ratio of the binder to the base material in the thermal insulation sheet of Example 3 is 2.9.
A thermal insulation sheet of Example 4 was produced in the same manner as in Example 1, except that the binder was changed and a urethane resin composition having a Tg of −12° C. and an elongation at break of 250% (“Evaphanol HA-190” produced by Nicca Chemical Co., Ltd.) was used. The elongation ratio of the binder to the base material in the thermal insulation sheet of Example 4 is 1.8.
A thermal insulation sheet of Example 5 was produced in the same manner as in Example 1, except that CMC (having a weight average molecular weight of 380,000) was added as a thickener in addition to the binder and silica aerogel in the production of the thermal insulation layer coating material. The addition amount of CMC was 3 parts by mass with respect to 100 parts by mass of the binder.
A thermal insulation sheet of Example 6 was produced in the same manner as in Example 1, except that glass fiber (having a fiber diameter of 6.5 μm) was added as a reinforcing fiber in addition to the binder and silica aerogel in the production of the thermal insulation layer coating material. The addition amount of glass fiber was 16 parts by mass with respect to 100 parts by mass of the binder.
A thermal insulation sheet of Example 7 was produced in the same manner as in Example 1, except that the material of the base material was changed. A polyimide film (“Kapton (registered trademark) 50H/V” produced by DuPont-Toray Co., Ltd., having a thickness of 12.5 μm and an elongation at break of 75%) was used as the base material. The elongation ratio of the binder to the base material in the thermal insulation sheet of Example 7 is 5.7.
A thermal insulation sheet of Example 8 was produced in the same manner as in Example 1, except that the material of the base material was changed. As the base material, an aluminum-deposited PET film (“Dialuster (registered trademark)” produced by Reiko Co., Ltd., having a thickness of 12 μm and an elongation at break of 100%) was used. The aluminum-deposited PET film was a laminate of a PET film layer (resin layer) and an aluminum-deposited layer (metal layer), and the thermal insulation layer was formed on the PET film layer side. The elongation ratio of the binder to the base material in the thermal insulation sheet of Example 8 is 4.3.
A thermal insulation sheet of Example 9 was produced in the same manner as in Example 1, except that the material of the base material was changed. A PPS film (“Torelina (registered trademark) #12-3K30” produced by Toray Industries, Inc., having a thickness of 12 μm and an elongation at break of 82%) was used as the base material. The elongation ratio of the binder to the base material in the thermal insulation sheet of Example 9 is 5.2.
A thermal insulation sheet of Example 10 was produced in the same manner as in Example 1, except that the material of the base material was changed. A cellophane film (“PL #300” produced by Futamura Chemical Co., Ltd., having a thickness of 25 μm and an elongation at break of 15%) was used as the base material. The elongation ratio of the binder to the base material in the thermal insulation sheet of Example 10 is 28.7.
A thermal insulation sheet of Example 11 was produced in the same manner as in Example 1, except that the D90 of silica aerogel used was changed. In the thermal insulation sheet of Example 11, silica aerogel pulverized in the same manner as in Example 1 was sieved using a sieve with an opening of 210 μm, and silica aerogel with D90 of 146 μm was used.
A thermal insulation sheet of Example 12 was produced in the same manner as in Example 1, except that the binder was changed and an acrylic resin composition having a Tg of −5° C. and an elongation at break of 280% (“AE982” produced by E-TEC) was used. The elongation ratio of the binder to the base material in the thermal insulation sheet of Example 12 is 2.0.
A thermal insulation sheet of Comparative Example 1 was produced in the same manner as in Example 1, except that the thickness of the base material was changed. A PET film having a thickness of 75 μm (“Lumirror #75” produced by Toray Industries, Inc., having an elongation at break of 150%) was used as the base material. The elongation ratio of the binder to the base material in the thermal insulation sheet of Comparative Example 1 is 2.9.
A thermal insulation sheet of Comparative Example 2 was produced in the same manner as in Example 1, except that the binder was changed and a urethane resin composition having a Tg of 72° C. and an elongation at break of 87% (“Superflex (registered trademark) 126 produced by Daiichi Kogyo Seiyaku Co., Ltd.) was used. The elongation ratio of the binder to the base material in the thermal insulation sheet of Comparative Example 2 is 0.6.
The state of the thermal insulation layer, bendability, and thermal insulation is evaluated for the produced thermal insulation sheet.
The surface of the thermal insulation layer immediately after being coated with the thermal insulation layer coated with the thermal insulation layer coating material and dried was visually observed to confirm the presence or absence of cracks, and the size and depth thereof when cracks were found. Regarding the state of the thermal insulation layer, when there were no cracks, the result was evaluated as extremely good (indicated by the mark in the evaluation column of Table 1 below), when there were cracks but the cracks were small, and the depth from the surface was less than 90% of the thickness of the thermal insulation layer, the result was evaluated as good (indicated by the mark ∘ in the same column), and when the cracks were large and the depth from the surface was 90% or more of the thickness of the thermal insulation layer, the result was evaluated as bad (indicated by the mark x in the same column).
One hour after the weight 52 was suspended from the thermal insulation sheet 50, the surface of the thermal insulation layer was visually observed to confirm the presence or absence of cracks, and the size and number of cracks when there were cracks. In addition, when there were no cracks, it was evaluated that the bendability was extremely excellent (indicated by the mark in the evaluation column of Table 1 below), when there were cracks but the size was small and the number of cracks were small, it was evaluated that the bendability was excellent (indicated by the mark ∘ in the same column), and when there were many cracks, it was evaluated that the bendability was poor (indicated by the mark x in the same column).
Five minutes after the thermal insulation sheet 60 was placed on the upper surface of the hot plate 61, the contact thermometer terminal 63 was brought into contact with the central part of the upper surface of the thermal insulation sheet 60 for 10 seconds, and the temperature during that time was measured. After that, the contact thermometer terminal 63 was brought into contact with the upper surface of the hot plate 61 for 10 seconds, and the temperature during that time was measured. The temperature difference (ΔT) was calculated by the following formula (i) using the maximum value among the temperatures measured at each.
ΔT (° C.)=(maximum value of hot plate temperature)−(maximum value of thermal insulation sheet temperature) (i)
Based on the calculated value of ΔT, thermal insulation was evaluated in three stages of high, medium, and low. That is, when ΔT was 25° C. or higher, it was evaluated that thermal insulation was “high” (indicated by the mark in the evaluation column of Table 1 below), when ΔT was 15° C. or higher to lower than 25° C., it was evaluated that thermal insulation was “medium” (indicated by the mark ∘ in the same column), and when ΔT was lower than 15° C., thermal insulation was evaluated as “low” (indicated by the mark x in the same column).
Table 1 summarizes the configuration and evaluation results of the thermal insulation sheets.
[μm]
0
[μm]
indicates data missing or illegible when filed
As shown in Table 1, according to the thermal insulation sheets of Examples 1 to 12, it was confirmed that the state of the thermal insulation layer was good, the bendability was excellent, and thermal insulation was “medium” or higher, and the practicality was high. The following description is based on the thermal insulation sheet of Example 1. In Example 2, since the thickness of the thermal insulation layer was large, the bendability was slightly lowered, but the thermal insulation layer was improved. In Example 3, the thickness of the base material was large, and thus the bendability was slightly reduced. In Examples 4 and 12, since the Tg of the binder was high and the elongation at break was small, the bendability was slightly lowered. In Example 5, the incorporation of CMC imparted flexibility to the thermal insulation layer. Therefore, cracks were less likely to occur when the thermal insulation layer coating material was dried or when the thermal insulation sheet was bent, and the state and bendability of the thermal insulation layer were improved. In Example 6, glass fibers were incorporated. Glass fibers were physically entangled around silica aerogel and served to reinforce the thermal insulation layer. Therefore, cracks were less likely to occur when the thermal insulation layer coating material was dried or when the thermal insulation sheet was bent, and the state and bendability of the thermal insulation layer were improved. In Examples 7 to 10, the material of the base material was different, but the state of the thermal insulation layer, the bendability, and thermal insulation was all approximately the same as in Example 1. In Example 11, silica aerogel containing particles with a higher D90, that is, a larger particle size than in Example 1, was used. Therefore, when the thermal insulation sheet is bent, cracks are unlikely to occur starting from the large particles, and thus it is considered that the bendability was slightly lowered. In this manner, it was confirmed that the thermal insulation sheet of the present disclosure was thin and excellent in flexibility such as bendability as well as thermal insulation.
On the other hand, in Comparative Example 1, the thickness of the base material is greater than 50 μm. Therefore, the heating from the base material side is not sufficient when drying the thermal insulation layer coating material, and heat is transferred unevenly in the coating film. As a result, the coating film swelled during drying, and many cracks occurred in the coating film (thermal insulation layer). Moreover, since the base material is thick, the rigidity is increased and the bending becomes difficult. Therefore, the stress applied to the thermal insulation layer during bending increased, and many cracks occurred. As a result, the heat transfer in the thermal insulation layer increased and thermal insulation decreased. In Comparative Example 2, a binder having a high Tg and a small elongation at break is used, and the elongation ratio of the binder to the base material is also small. Therefore, the thermal insulation layer lacked flexibility, and many cracks occurred both after drying and during bending. As a result, the heat transfer in the thermal insulation layer increased and thermal insulation decreased.
The thermal insulation sheet of the present disclosure can be applied to various parts and members in the fields of automobiles, logistics, housing, industrial equipment, information communication equipment, and the like. The automotive field includes interior parts such as door trims, ceiling materials, instrument panels, console boxes, and armrests; and members such as hoses and pipes. In the field of logistics, there are thermally insulated containers used for transporting food, pharmaceuticals, and the like. The housing field includes building materials, wall materials, attic materials, window sashes, and the like. In the field of industrial equipment, thermal insulation members used in motors, sensors, and the like can be mentioned. In the field of information and communication equipment, thermal insulation members used in personal computers and smartphones can be mentioned. In addition, it is suitable for thermal insulation members for shoes such as insoles, and daily necessities such as cooler boxes.
| Number | Date | Country | Kind |
|---|---|---|---|
| 2021-096290 | Jun 2021 | JP | national |
This application is a continuation of PCI International Application No. PCT/JP2022/022256, filed on Jun. 1, 2022, which claims priority under 35 U.S.C § 119(a) to Japanese Patent Application No. 2021-096290, filed on Jun. 9, 2021. Each of the above application(s) is hereby expressly incorporated by reference, in its entirety, into the present application.
| Number | Date | Country | |
|---|---|---|---|
| Parent | PCT/JP2022/022256 | Jun 2022 | US |
| Child | 18446492 | US |
