Summary of the invention
The object of the present invention is to provide a kind of have excellent weathering resistance, yellowing resistance energy, flame retardant properties, the de-oxime type silicone sealant single-component room-temperature vulcanized, that seal for solar module that water vapor transmission rate (WVTR) is low and stable storing performance is good.
For achieving the above object, the invention provides following technical scheme:
The de-oxime type silicone sealant of single component of solar module sealing, is characterized in that sealing glue is comprised of by following weight parts following component:
Viscosity is 20000~80000 α, 100 parts of alpha, omega-dihydroxy polydimethyl siloxanes;
1~6 part of polyisobutene resin;
10~50 parts of activated Calcium carbonates;
1~15 part, silicone oil softening agent;
10~40 parts of fire retardants;
1~5 part of titanium dioxide;
Specific surface area is 1~7 part of 130m2/g gas-phase silica;
9~15 parts of linking agents;
2~5 parts of silane coupling agents;
0.5~1.5 part of catalyzer.
It is 10000~40000 poly-isobutyl-resin that the poly-isobutyl-resin of above-mentioned use is preferably number-average molecular weight.
The activated Calcium carbonate of above-mentioned use can outsourcing, as Shaanxi Hai Ze nano material company limited etc.As preferred mode, can, by the conventional method of the industry, with resinous acid, process activated Calcium carbonate before use.
Above-mentioned linking agent preferably in methyl three isobutyl ketone oximino silanes, vinyl three isobutyl ketone oximino silanes and four isobutyl ketone oximino silanes a kind of, two or three.
Above-mentioned catalyzer is a kind of, two or more combination in dibutyl tin laurate, dibutyl tin acetate, stannous octoate and dibutyl two stannous octoates preferably.
Above-mentioned silane coupling agent is selected from a kind of, two or more combination in γ-methacryloxypropyl trimethoxy silane, γ-glycidyl ether oxygen propyl trimethoxy silicane, γ-aminopropyl triethoxysilane, vinyl three ('beta '-methoxy oxyethyl group) silane and two (γ-trimethoxy-silylpropyl) amine.
A kind of, two or more combination in aluminium hydroxide, magnesium hydroxide, antimonous oxide, zinc subcarbonate, zinc borate, trimeric cyanamide, trimeric cyanamide phosphoric acid ester, melamine cyanurate, Resorcinol two (hexichol phosphoric acid ester) and ammonium polyphosphate that above-mentioned fire retardant is preferably hung oneself after silane coupling agent processing.
The size that above-mentioned titanium dioxide is preferably particulate is less than the titanium dioxide of 100 nanometers.
Above-mentioned silicone oil softening agent is preferably the polydimethylsiloxane that molecular end is methyl, and its viscosity in the time of 25 ℃ is 0.5~2.0 Pa.s.
Above-mentioned specific surface area is that the specific surface area of 130m2/g gas-phase silica is preferably 90~200cm
3/ g.
The present invention also provides a kind of preparation method of the above-mentioned de-oxime type silicone sealant of single component for solar module sealing, it is characterized in that comprising the following steps:
(1) by specific surface area, be 90~200cm
3the specific surface area of/g is that 130m2/g gas-phase silica is at 65~180 ℃ of drying and dewatering 2-3 hour;
(2) α that is 20000~80000 by viscosity, alpha, omega-dihydroxy polydimethyl siloxane 100 weight parts, polyisobutene resin 1~6 weight part, activated Calcium carbonate 10~40 weight parts, silicone oil softening agent 1~15 weight part, aluminium hydroxide 10~40 weight parts, titanium dioxide 1~5 weight part, adds in vacuum kneader, in 65~180 ℃ of temperature, vacuum tightness, is 0.06~0.1MPa, blend dehydration 60~180 minutes, the cooling base-material that obtains;
(3) at room temperature, by the specific surface area after step (1) dehydration, be 130m2/g gas-phase silica 1~7 weight part again, linking agent 9~15 weight parts, silane coupling agent 2~5 weight parts, catalyzer 0.5~1.5 weight part, adds in the high speed dispersion planet machine that above-mentioned base-material is housed, in rotating speed 40~60rpm, vacuum tightness 0.06~0.1 MPa stirs 30~150 minutes, makes the de-oxime type silicone sealant of single component.
Embodiment
Below in conjunction with specific embodiment, the present invention is further described, but does not limit the invention to these embodiments.One skilled in the art would recognize that the present invention contained all alternativess, improvement project and the equivalents that within the scope of claims, may comprise.
embodiment 1
By specific surface area, be 130 cm
3/ g gas-phase silica was 110 ℃ of drying and dewaterings 2 hours; The α that is 20000cPa.s by viscosity, 100 parts of alpha, omega-dihydroxy polydimethyl siloxanes, 10 parts of the methyl-silicone oils that the polydimethylsiloxane viscosity that molecular end is methyl is 1000cPa.s, 5 parts of polyisobutene resins, 30 parts of activated Calcium carbonates, 25 parts, aluminium hydroxide, 5 parts of zinc subcarbonates, 2 parts of ammonium polyphosphates, particle size is that 3 parts of the titanium dioxides of 0.08 micron add in vacuum kneader, in 110 ℃ of temperature, vacuum tightness, be 0.07MPa, blend dehydration 150 minutes, the cooling base-material that obtains.At room temperature, then be 130m by specific surface area
25 parts of/g gas-phase silicas, 8 parts of methyl three isobutyl ketone oximino silanes, 5 parts of vinyl three isobutyl ketone oximino silanes, four 0.5 part of isobutyl ketone oximino silane, 3 parts, vinyl three ('beta '-methoxy oxyethyl group) silane, 1 part of two (γ-trimethoxy-silylpropyl) amine, 1.1 parts of dibutyl tin laurates, add in the high speed dispersion planet machine that above-mentioned base-material is housed, in rotating speed 60rpm, vacuum tightness 0.08MPa, stirs 60 minutes, make the de-oxime type silicone sealant of single component, product performance test result is in Table 1.
embodiment 2
By specific surface area, be 200cm
3/ g gas-phase silica was 110 ℃ of drying and dewaterings 3 hours; The α that is 50000cPa.s by viscosity, 100 parts of alpha, omega-dihydroxy polydimethyl siloxanes, 10 parts of the methyl-silicone oils that the polydimethylsiloxane viscosity that molecular end is methyl is 1000cPa.s, 1 part of polyisobutene resin, 30 parts of activated Calcium carbonates, 25 parts, aluminium hydroxide, 5 parts of zinc subcarbonates, 2 parts of ammonium polyphosphates, particle size is that 3 parts of the titanium dioxides of 0.08 micron add in vacuum kneader, in 110 ℃ of temperature, vacuum tightness, be 0.07MPa, blend dehydration 150 minutes, the cooling base-material that obtains.At room temperature, then be 200cm by specific surface area
35 parts of/g gas-phase silicas, 12 parts of methyl three isobutyl ketone oximino silanes, 2 parts of vinyl three isobutyl ketone oximino silanes, 3 parts, vinyl three ('beta '-methoxy oxyethyl group) silane, 1 part of two (γ-trimethoxy-silylpropyl) amine, 1.1 parts of dibutyl tin laurates, add in the high speed dispersion planet machine that above-mentioned base-material is housed, in rotating speed 60rpm, vacuum tightness 0.08MPa, stir 60 minutes, make the de-oxime type silicone sealant of single component, product performance test result is in Table 1.
embodiment 3
By specific surface area, be 130cm
3/ g gas-phase silica was 110 ℃ of drying and dewaterings 2 hours; The α that is 80000cPa.s by viscosity, 100 parts of alpha, omega-dihydroxy polydimethyl siloxanes, molecular end is 15 parts of the polydimethylsiloxane viscosity of the methyl methyl-silicone oils that is 1000cPa.s, 5 parts of polyisobutene resins, 40 parts of activated Calcium carbonates, 20 parts, aluminium hydroxide, 15 parts of zinc subcarbonates, particle size is that 3 parts of the titanium dioxides of 0.08 micron add in vacuum kneader, in 110 ℃ of temperature, vacuum tightness, is 0.07MPa, blend dehydration 150 minutes, the cooling base-material that obtains.At room temperature, then be 130cm by specific surface area
33 parts of/g gas-phase silicas, 8 parts of methyl three isobutyl ketone oximino silanes, 5 parts of vinyl three isobutyl ketone oximino silanes, four 0.5 part of isobutyl ketone oximino silane, 1.5 parts of γ-aminopropyl triethoxysilanes, 1.0 parts of two (γ-trimethoxy-silylpropyl) amine, 1.0 parts of dibutyl tin laurates, add in the high speed dispersion planet machine that above-mentioned base-material is housed, in rotating speed 60rpm, vacuum tightness 0.08MPa, stirs 60 minutes, make the de-oxime type silicone sealant of single component, product performance test result is in Table 1.
embodiment 4
By specific surface area, be 130cm
3/ g gas-phase silica was 110 ℃ of drying and dewaterings 2 hours; The α that is 80000cPa.s by viscosity, 100 parts of alpha, omega-dihydroxy polydimethyl siloxanes, molecular end is 15 parts of the polydimethylsiloxane viscosity of the methyl methyl-silicone oils that is 1000cPa.s, 5 parts of polyisobutene resins, 40 parts of activated Calcium carbonates, 45 parts, the aluminium hydroxide of processing through silane coupling agent, particle size is that 3 parts of the titanium dioxides of 0.08 micron add in vacuum kneader, in 110 ℃ of temperature, vacuum tightness, be 0.07MPa, blend dehydration 150 minutes, the cooling base-material that obtains.At room temperature, then be 130cm by specific surface area
33 parts of/g gas-phase silicas, 8 parts of methyl three isobutyl ketone oximino silanes, 5 parts of vinyl three isobutyl ketone oximino silanes, four 0.5 part of isobutyl ketone oximino silane, 1.5 parts of γ-aminopropyl triethoxysilanes, 1.0 parts of two (γ-trimethoxy-silylpropyl) amine, 1.0 parts of dibutyl tin laurates, add in the high speed dispersion planet machine that above-mentioned base-material is housed, in rotating speed 60rpm, vacuum tightness 0.08MPa, stirs 60 minutes, make the de-oxime type silicone sealant of single component, product performance test result is in Table 1.
embodiment 5
By specific surface area, be 130cm
3/ g gas-phase silica was 110 ℃ of drying and dewaterings 3 hours; The α that is 50000cPa.s by viscosity, 100 parts of alpha, omega-dihydroxy polydimethyl siloxanes, molecular end is 10 parts of the polydimethylsiloxane viscosity of the methyl methyl-silicone oils that is 1000cPa.s, 1 part of polyisobutene resin, 30 parts of activated Calcium carbonates, 25 parts, the aluminium hydroxide of processing through silane coupling agent, 20 parts of ammonium polyphosphates, particle size is that 3 parts of the titanium dioxides of 0.06 micron add in vacuum kneader, in 110 ℃ of temperature, vacuum tightness, is 0.07MPa, blend dehydration 150 minutes, the cooling base-material that obtains.At room temperature, then be 130cm by specific surface area
35 parts of/g gas-phase silicas, 12 parts of vinyl three isobutyl ketone oximino silanes, 3 parts, vinyl three ('beta '-methoxy oxyethyl group) silane, 1 part of two (γ-trimethoxy-silylpropyl) amine, 1.1 parts of dibutyl tin laurates, add in the high speed dispersion planet machine that above-mentioned base-material is housed, in rotating speed 60rpm, vacuum tightness 0.08MPa, stirs 60 minutes, make the de-oxime type silicone sealant of single component, product performance test result is in Table 1.
comparing embodiment 1
By specific surface area, be 130cm
3/ g gas-phase silica was 110 ℃ of drying and dewaterings 3 hours; The α that is 20000cPa.s by viscosity, 100 parts of alpha, omega-dihydroxy polydimethyl siloxanes, molecular end is 10 parts of the polydimethylsiloxane viscosity of the methyl methyl-silicone oils that is 1000cPa.s, 30 parts of activated Calcium carbonates, 25 parts, the aluminium hydroxide that silane coupling agent was processed, 5 parts of zinc subcarbonates, particle diameter is that 3 parts of the titanium dioxides of 0.08 micron add in vacuum kneader, in 110 ℃ of temperature, vacuum tightness, be 0.07MPa, blend dehydration 150 minutes, the cooling base-material that obtains.At room temperature, then be 130cm by specific surface area
31 part of/g gas-phase silica, 8 parts of methyl three isobutyl ketone oximino silanes, 5 parts of vinyl three isobutyl ketone oximino silanes, four 0.5 part of isobutyl ketone oximino silane, 3 parts, vinyl three ('beta '-methoxy oxyethyl group) silane, 1 part of two (γ-trimethoxy-silylpropyl) amine, 1.1 parts of dibutyl tin laurates, add in the high speed dispersion planet machine that above-mentioned base-material is housed, in rotating speed 60rpm, vacuum tightness 0.08MPa, stirs 60 minutes, make the de-oxime type silicone sealant of single component, product performance test result is shown in Table 1.
comparing embodiment 2
By specific surface area, be 130cm
3/ g gas-phase silica was 110 ℃ of drying and dewaterings 2 hours; The α that is 50000cPa.s by viscosity, 100 parts of alpha, omega-dihydroxy polydimethyl siloxanes, molecular end is 10 parts of the polydimethylsiloxane viscosity of the methyl methyl-silicone oils that is 1000cPa.s, 30 parts of activated Calcium carbonates, 25 parts, the aluminium hydroxide that silane coupling agent was processed, 5 parts of zinc subcarbonates, add in vacuum kneader, in 110 ℃ of temperature, vacuum tightness, be 0.07MPa, blend dehydration 150 minutes, the cooling base-material that obtains.At room temperature, then be 130cm by specific surface area
35 parts of/g gas-phase silicas, 12 parts of methyl three isobutyl ketone oximino silanes, 5 parts of vinyl three isobutyl ketone oximino silanes, 3 parts of γ-aminopropyl triethoxysilanes, 1 part of two (γ-trimethoxy-silylpropyl) amine, 0.8 part of dibutyl tin laurate, adds in the high speed dispersion planet machine that above-mentioned base-material is housed, in rotating speed 60rpm, vacuum tightness 0.08MPa, stir 60 minutes, make the de-oxime type silicone sealant of single component, product performance test result is shown in Table 1.
Table 1 seal gum the performance test results
Sequence number |
Project |
Embodiment 1 |
Embodiment 2 |
Embodiment 3 |
Embodiment 4 |
Embodiment 5 |
Comparative example 1 |
Comparative example 2 |
1 |
Surface drying time |
11 |
13 |
13 |
12 |
10 |
15 |
10 |
2 |
Shore hardness (Shore A) |
36 |
38 |
37 |
38 |
36 |
39 |
35 |
3 |
Tensile strength (MPa) |
≥2.0 |
≥2.0 |
≥1.8 |
≥1.8 |
≥1.8 |
≥1.6 |
≥1.6 |
4 |
Thermal ageing (be full of cracks) |
Nothing |
Nothing |
Nothing |
Nothing |
Nothing |
Nothing |
Nothing |
5 |
Flame retardant rating |
FV-0 |
FV-0 |
FV-0 |
FV-0 |
FV-0 |
FV-0 |
FV-1 |
6 |
Volume specific resistance (Ω cm
3)
|
≥1.5×10
13 |
≥1.5×10
13 |
≥1.5×10
13 |
≥1.5×10
13 |
≥1.5×10
13 |
≥1.5×10
13 |
≥ ≥1.5×10
13 |
7 |
Dielectric strength (KV/mm) |
≥16 |
≥16 |
≥16 |
≥16 |
≥16 |
≥16 |
≥16 |
8 |
With anodised aluminium adhesive property |
Cohesive failure |
Cohesive failure |
Cohesive failure |
Cohesive failure |
Cohesive failure |
Cohesive failure |
Cohesive failure |
9 |
With glassy bond performance |
Cohesive failure |
Cohesive failure |
Cohesive failure |
Cohesive failure |
Cohesive failure |
Cohesive failure |
Cohesive failure |
10 |
With PPO/PA cohesiveness |
Cohesive failure |
Cohesive failure |
Cohesive failure |
Cohesive failure |
Cohesive failure |
Cohesive failure |
Cohesive failure |
11 |
Yellowing resistance |
Xanthochromia not |
Xanthochromia not |
Xanthochromia not |
Xanthochromia not |
Xanthochromia not |
Xanthochromia not |
Xanthochromia |
12 |
Vapor permeability (g/m
2.d)
|
6 |
8 |
6 |
7 |
7 |
28 |
29 |
13 |
Storage period (moon) |
9 |
9 |
9 |
9 |
9 |
9 |
9 |